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1 McKEE, R. M., An Experimental Study of the Interaction of a Plane Shock Wave with a Contact Region. Sept. 1954

2 WALDRON, H. F., An Experimental Study of a Spiral Vortex Formed by Shock-Wave Diffraction. Sept. 1954

3 WILSON, L. N., An Experimental Investigation of Reynolds Number Effects on Supersonic Static Probes. Sept. 1954

4 ENKENHUS, K. R. and TUCKER, N. B., Design and Testing of an Axi-Symmetric Flow Nozzle for Mach Number Seven. Jan. 1955

5 BILLINGTON, I. J., The Hot-Wire Anemometer and Its Use in Non-Steady Flow. Jan. 1955

6 HARRIS, E. L., Investigation of the Time Response and Outgassing Effects of Pressure Probes in Free-Molecule Flow. Oct. 1955

7 WATTS, G. A., An Experimental Investigation of a Sonic Jet Directed Upstream Against a Uniform Supersonic Flow. Jan. 1956

8 BOYER, D. W., Effects of Kinematic Viscosity and Wave Speed on Shock Wave Attenuation. May 1956

9 LUDWIG, G. R., Effects of Probe Size on Measurements in a Laminar Boundary Layer in Supersonic Flow. Nov. 1956

10 SREEKANTH, A. K., Performance of a Mach 4 Axially Symmetric Nozzle Designed to Operate at 40 Microns Hg. in the UTIA Low-Density Wind Tunnel. Sept. 1956

11 BRENCKMANN, M., Experimental Investigations of the Aerodynamics of a Wing in a Slipstream. April 1957

12 WOLFF, E. R., The Development of a Mass Flow Probe. Jan. 1957

13 FRANKS, W. J., Interactions of a Shock Wave with a Wire Screen. May 1957

14 McGREGOR, D. M., An Experimental Investigation of the Oscillating Pressures on a Circular Cylinder in a Fluid Stream. June 1957

15 CAMPBELL, A. J., Investigation of a Wide Angle Diffuser with Air Augmentation for Use as a Jet Muffler. Aug. 1957

16 MURRAY, J. B., An Experimental Investigation of Temperature and Pressure Recovery, Running Time and Blockage Characteristics of the UTIAS 16 in. x 16 in. Supersonic Wind Tunnel. Aug. 1957

17 GALEZOWSKI, S. H., Effects of Probe Tip Geometry and Size on Measurement in a Laminar Boundary Layer in Supersonic Flow. Oct. 1957

18 BROWN, D., An Experimental Investigation of the Pressure Recovery of a Perforated-Wall Internal-Compression Intake at a Free-Stream Mach Number of 2.5. May 1957

19 RIBNER, H. S., On the Lift and Induced Drag Associated with Large Downwash Angles. Jan. 1958

20 MAESTRELLO, L., UTIA Air Duct Facility for Investigation of Vibration Noise Induced by Turbulent Flow Past a Panel (Boundary Layer Noise). April 1958

21 RIBNER, H. S., Note on Acoustic Energy Flow in a Moving Medium. April 1958

22 MUNTZ, E. P., Pressure Measurements in Free Molecule Flow with a Rotating Arm Apparatus. May 1958

23 PRENDERGAST, V. D., Measurement of Two-Point Correlations of the Surface Pressure on a Circular Cylinder. July 1958

24 CLARK, J.P.C., An Experimental Investigation of a Supersonic Two-Dimensional Perforated Inlet at a Nominal Free Stream Mach Number of 2.5. Nov. 1958

25 FRIEND, W. H., The Interaction of a Plane Shock Wave with an Inclined Perforated Plate. Oct. 1958

26 DE LEEUW, J. H., GLASS, I. I. and HEUCKROTH, L. E., A High-Speed Multi-Source Spark Camera. Feb. 1962

27 TAYLOR, B. W., Development of Thin Film Heat Transfer Gauges for Shock Tube Flows. June 1959

28 DATAR, S., Temperature Response of a Hot-Wire Anemometer to Shock and Rarefaction Waves. June 1959

29 KURYLOWICH, G., The Applicability of a Sine-Series Velocity Profile in a Two-Dimensional Incompressible Laminar Boundary Layer. July 1959

30 GLASS, I. I., HEUCKROTH, L. E. and MOLDER, S., On the One-Dimensional Overtaking of a Shock Wave by a Rarefaction Wave. July 1959

31 EL BAROUDI, M. Y., Measurement of Two-Point Correlations of Velocity Near a Circular Cylinder Shedding a Karman Vortex Street. Jan. 1960

32 ETKIN, B., A Simple Method for the Analogue Computation of the Mean Square Response of Airplanes to Atmospheric Turbulence. Jan. 1960

33 BREMNER, G. F., DUKOWICZ, J. K. and GLASS, I. I., On the One-Dimensional Overtaking of a Rarefaction Wave by a Shock Wave. Feb. 1960

34 FRENCH, J. B. and MUNTZ, E. P., Design Study of the UTIA Plasma Tunnel. March 1960

35 SWANSON, S. R., Systematic Axial-Load Fatigue Tests Using Unnotched Aluminum Alloy 2024S-T4 Extruded Bar Specimens. May 1960

36 POPPLETON, E. D., A Note on the Design of Redundant Structures. July 1960

37 GARLAND, D. B., Studies of Ground Effect on Conical Annular Jet. Aug. 1960

38 MOLDER, S., Head-On Interaction of Oblique Shock Waves. Sept. 1960

39 CHISHOLM, R.G.A., Design and Calibration of an Air Ejector to Operate Against Various Back Pressures. Sept. 1960

40 RANGI, R. S., Nonlinear Effects in the Longitudinal Dynamics of a Lifting Vehicle in a Circular Orbit. Oct. 1960

41 SODERQUIST, A.B.T., Experimental Investigation of Stability and Post Buckling Behaviour of Stiffened Curved Plates. Sept. 1960

42 ROBERTS, A. K., Design of the Recoil System for the 4" x 7" Hypersonic Shock Tube. Oct. 1960

43 COLLINS, R., Some Methods of Generating Cylindrical Explosions. Nov. 1960

44 WONG, H.Y.T., A Preliminary Investigation of Use of Flow Expanders to Generate Hypersonic Flow in a Wind Tunnel. Oct. 1960

45 McCLEAN, R., The Optimization of an Autopilot for an Airplane Subjected to Random Atmospheric Turbulence. Nov. 1960

46 POPPLETON, E. D., Note on the Matrix Analysis of Nonlinear Structures. March 1961

47 SMITH, R. E., Studies of Ground Effect on a 60[[ring]] Inwardly Inclined Annular Jet, Part II. May 1961

48 FINE, J. H., Stability of Flight Paths of Lifting Vehicles During Entry into Planetary Atmospheres. July 1961

49 BAILEY, A. B., Use of the Coanda Effect for the Deflection of Jet Sheets Over Smoothly Curved Surfaces, Part I. Aug. 1961

50 DAU, K., Wind Tunnel Tests of the Toronto City Hall, July 1961

51 RODERICK, W., Use of the Coanda Effect for the Deflection of Jet Sheets Over Smoothly Curved Surfaces, Part II. Sept. 1961

52 DUKOWICZ, J. K., The Efficiency of Energy Transfer Associated with Magnetically Driven Shock Waves in a Tee-Tube. April 1963

53 LIIVA, J., A Facility for Dynamic Testing of Models of Airborne Vehicles with Ground Effect. Oct. 1961

54 CARR, J. B., Analysis of the Performance of the UTIA Random Load Fatigue Facility. Oct. 1961

55 KURYLOWICH, G., Investigation of the Oscillatory Derivatives of an Aerofoil with Flaps Oscillating at Negative Angles of Attack. Oct. 1961

56 DAU, K., Characteristics of a Rectangular Wing with a Peripheral Jet in Ground Effect, Part I. Sept. 1961

57 TENNYSON, R. C., An Experimental Investigation of the Behaviour of Stiffened Plates in Axial Compression. Sept. 1961

58 SONIN, A. A., Langmuir Probe Measurements in the Stagnation Point Boundary Layer of a Blunt Nosed Body in a Supersonic Plasma Flow. June 1963

59 DAVIS, J., Characteristics of a Rectangular Wing with a Peripheral Jet in Ground Effect, Part II. May 1962

60 LIIVA, J., Gyrostabilization of an Elliptic Wing with Peripheral Jet Hovering in Ground Effect. Aug. 1962

61 SCOTT, W. J., Asymmetry of Annular Jet Flow in Ground Proximity, Part I. May 1962

62 BILLINGTON, I. J., FAVREAU, R. F., GLASS, I. I. and HEUCKROTH, L.E., Some Experiments on the Use of Large Glass Panels as Emergency Pressure Relief Diaphragms. Aug. 1962

63 STEPHENS, P. R., Asymmetry of Annular Jet Flow in Ground Proximity - Part II. Oct. 1962

64 RADFORD, R. C., Development of a Propulsion System for Powering a Self-Propelled GETOL Model Aircraft. Dec. 1962

65 ETKIN, B. and MACKWORTH, J., Aerodynamic Instability of Non-Lifting Bodies Towed Beneath an Aircraft. Jan. 1963

66 MAK, W. H., Sodium Line Reversal Temperature Measurements in Shock-Tube Flows. May 1963

67 LAFRANCE, J. C., Pressure Measurement in Transition and Free Molecular Flows Using Orifice Probes. June 1963

68 DUKOWICZ, J., The Flat-Plate Magnetohydrodynamic Boundary Layer in a Transverse Magnetic Field. Jan. 1967

69 GALIPEAU, J. and TAKANO, A., A Digital Computer Program for Calculating Nonequilibrium Expansion Flows of Dissociated Oxygen and Ionized Argon Around a Corner. Aug. 1963 (Also AFOSR Report 64-0075)

70 HOPE-GILL, C. D., An Experimental Investigation into the Shape of Thrust-Augmenting Surfaces in Conjunction with Coanda Deflected Jet Sheets. Oct. 1963

71 BENOIT, A., An Experimental Investigation of Spherical Combustion for the UTIA Implosion Driven Launcher. Sept. 1963

72 SIMPSON, B., Pressure Measurements in Low-Energy Underwater Explosions. Sept. 1963

73 CICCI, F., An Investigation of the Statistical Distribution of Constant Amplitude Fatigue Endurances for a Maraging Steel. July 1964

74 GOWANS, B. W., Experimental Study of the Aerodynamic Characteristics of a Model of an Air Cushion Vehicle in Hovering Flight. Feb. 1964

75 O'KEEFE, D. R., Initial Performance Study of the UTIAS High Energy Molecular Beam Facility. Sept. 1964

76 UNPUBLISHED

77 SURRY, D., Characteristics of a Rectangular Wing with a Peripheral Jet in Ground Effect, Part III. Sept. 1964

78 BENNER, S. D., The Coanda Effect at Deflection Surfaces Widely Separated from the Jet Nozzle. April 1965

79 MEHUS, T. E., An Experimental Investigation into the Shape of Thrust Augmenting Surfaces in Conjunction with Coanda-Deflected Jet Sheets (Part II). Jan. 1965

80 PRINCE, R. H., A Low Energy Nitrogen Ion Beam. May 1965

81 UNPUBLISHED

82 NISHIMURA, Y., Application of a Jet Pump and Coanda Surface to Ventilation of Highway Tunnel. Feb. 1964

83 MAKOMASKI, A. H., Preliminary One-Dimensional Investigation of the Initiation of Low-Density PETN by Hydrogen-Oxygen Detonation Waves. Feb. 1965

84 WALENTA, Z. A., Analogue Networks for High Heat-Transfer Rate Measurements. Nov. 1964 (Also AFOSR Report 65-0261)

85 BENOIT, A., Thermodynamic and Composition Data for Constant-Volume Combustion of Stoichiometric Mixtures of Hydrogen-Oxygen Diluted with Helium or Hydrogen. Nov. 1964

86 MASAK, M., On the Lateral Instabilities of Aircraft Due to Parametric Excitation. Jan. 1965

87 FEIR, J. B., The Effects of an Arrangement of Vortex Generators Installed to Eliminate Wind Tunnel Diffuser Separation. June 1965

88 SIDDON, T. E., A Turbulence Probe Utilizing Aerodynamic Lift. May 1965

89 SURRY, J., Experimental Investigation of the Characteristics of Flow About Curved Circular Cylinders. April 1965

90 DREWRY, J. E. and WALENTA, Z. A., Determination of Diaphragm Opening-Times and Use of Diaphragm Particle Traps in a Hypersonic Shock Tube. May 1965

91 CHAN, Y. Y., MASON, R. P. and REDDY, N. M., Instrumentation and Calibration of UTIAS Hypersonic Shock Tunnel. June 1965 (Also AFOSR Report 66-0002)

92 HUGHES, P. C., Subsonic Tests in Free Molecule Flow on Impact Tube Pressure Probes Having a Wide Range of Tube Lengths at Angles of Attack up to 90[[ring]]. June 1965

93 FLAGG, R. F., A Theoretical Analysis of the Driver-Reservoir Method of Driving Hypersonic Shock Tunnels. July 1965

94 TIRUMALESA, D., Sonic Line in Nonequilibrium Flows. July 1965

95 REID, L. D., The Design of a Facility for the Measurement of Human Pilot Dynamics. June 1965

96 FILOTAS, L. T., Distortion of a Shock Wave Traversed by a Vortex. Jan. 1967

97 GORJUP, M., Calibration of a Micrometeoroid Impact. March 1967

98 UNPUBLISHED

99 KENNEDY, J. E. and GLASS, I. I., Multipoint Initiated Implosions from Hemispherical Shells of Sheet Explosive. Dec. 1966

100 GARAY, E. K., Effect of Ground Board Boundary Layer on Air Cushion Vehicles Wind Tunnel Tests. Jan. 1967

101 ELLIS, N. D., A Computer Study of a Wing in a Slipstream. Feb. 1967

102 BENOIT, A., Specific Heat Ratios and Isentropic Exponents for Constant Volume Combustion of Stoichiometric Mixtures of Hydrogen-Oxygen Diluted with Helium or Hydrogen. Dec. 1966

103 DE LEEUW, J. H. and GADAMER, E. O., Density Distribution of a Molecular Flux from a Short Cylindrical Tube. Feb. 1967

104 BENOIT, A., Properties of Chapman-Jouguet Detonations in Stoichiometric Hydrogen-Oxygen Mixtures Diluted with Helium and Hydrogen. Dec. 1966

105 ANDERSON, J.H.B., An Experimental Determination of the Gladstone-Dale Constants for Dissociating Oxygen. March 1967

106 SIMPSON, R., The Training of Subjects for UTIAS Research on Dynamics of Human Pilots. March 1967

107 STRONG, D. R., SIDDON, T. E. and CHU, W. T., Pressure Fluctuations on a Flat Plate with Oblique Jet Impingement. Feb. 1967

108 RIBNER, H. S., Acoustic Energy Flux from Shock-Turbulence Interaction. July 1967

109 ATVARS, J., SCHUBERT, L. K., GRANDE, E. and RIBNER, H. S., Refraction of Sound by Jet Flow or Jet Temperature. May 1965 (superseded by NASA CR-494)

110 GRANDE, E., Refraction of Sound by Jet Flow and Jet Temperature II. Dec. 1966

111 MUGGERIDGE, D. B., An Attempt to Correlate Bimodal Fatigue Endurance Distributions in OFHC Copper with Wood's H, F and S Ranges. June 1967

112 HAAGENSEN, P. J., Statistical Aspects of Coexisting Fatigue Failure Mechanisms in OFHC Copper. June 1967

113 WATSON, J. D., Implosion Driven Hypervelocity Launcher Performance Using Gaseous Detonation Waves. May 1967

114 TIRUMALESA, D., Discontinuous Solutions for Nonequilibrium Supersonic Flows. June 1967

115 CAMPBELL, A. C. and ETKIN, B., The Response of a Cylindrical Structure to a Turbulent Flow Field at Subcritical Reynolds Number. July 1967

116 SURRY, J. and SURRY, D., The Effect of Inclination of the Strouhal Number and Other Wake Properties of Circular Cylinders at Subcritical Reynolds Numbers. Aug. 1967

117 OOSTHUIZEN, P. H., An Analysis of the Interaction of a Boundary Layer and the Corner-Expansion Wave in Supersonic Flow. Aug. 1967

118 CASE, E. R., A Study of the Effects of CL-Coupling on the Lateral Stability of Aircraft in Atmospheric Turbulence. Sept. 1967

119 LEVY, A., Preliminary Temperature Measurements Behind Strong Shock Waves in Argon. Sept. 1967

120 TIRUMALESA, D., Oxygen Corner-Expansion Flows with Coupled Vibrational and Dissociational Nonquilibrium. Dec. 1967

121 SEVRAY, P., Performance Analysis of UTIAS Implosion-Driven Hypervelocity Launcher. Jan. 1968

122 STUBBE, E. J., Magnetohydrodynamic Flow Near a Stagnation Point. Jan. 1968

123 RAVINDRAN, R., Statistical and Metallographic Aspects of Fatigue Failure Mechanisms in Metals. Feb. 1968

124 KNAPP, W., The Effects of Specimen Grain Size and Environment on the Fatigue Life of OFHC Copper. June 1968

125 McLEOD, M. G., A Spinning Hot-Wire Anemometer for Simultaneous Measurement of u, v and w. March 1968

126 WEYNANTS, R. R., An Experimental Investigation of Shock-Wave Diffraction over Compression and Expansion Corners. April 1968

127 HUGHES, P. C., Geometrical Properties in State Space of Linear Differential Equations with Periodic Coefficients. July 1968

128 BENOIT, A., Equilibrium Thermodynamic Data for the H2-O2-He Systems. Aug. 1968

129 SULLIVAN, P. A., On the Interaction of a Laminar Hypersonic Boundary Layer and a Corner Expansion Wave. Aug. 1968

130 FLAGG, R. F. and MITCHELL, G. P., An Optimization Study of the UTIAS Implosion-Driven Hypervelocity Launcher MK II. Dec. 1968

131 NAYAR, B. M., SIDDON, T. E. and CHU, W. T., Properties of the Turbulence in the Transition Region of a Round Jet. Jan. 1969

132 GARG, S. K., Spherical Elastic-Plastic Waves in Solid Media. Feb. 1969

133 TEUNISSEN, H. W., An Ejector-Driven Wind Tunnel for the Generation of Turbulent Flows with Arbitrary Mean Velocity Profile. Feb. 1969

134 MIDDLETON, D. and CLARK, P.J.F., Assessment and Development of Methods of Acoustic Performance Prediction for Jet Noise Suppressors. April 1969

135 GARG, S. C., On the Use of Strings and Wires in Gravity-Gradient Stabilization Systems: Orbit Plane Analysis. June 1969

136 POINSSOT, J. C., A Preliminary Investigation of a UTIAS Implosion-Driven Shock Tube. July 1969

137 CHERCHAS, D. B., Spin Decay of a Class of Satellites Caused by Solar Radiation. Part II: Arbitrary Attitude of the Spin Axis. July 1969

138 NIRANJAN, V., Bonded Joints -- A Photoelastic Study. July 1970

139 COOPER, K. R., Bending Response of a Cantilever Cylinder to Turbulent Shear Flow. Sept. 1969

140 ROBERTS, D. E., A Spectroscopic Investigation of Combustion-Driven Spherical Implosion Waves. Aug. 1969

141 McLEOD, M. G., A Comprehensive Survey of Passengers Flying from Toronto International Airport May-June 1968. Aug. 1969

142 PUCCINI, R., Fatigue Tests and Microstructural Studies of OFHC Copper from 25[[ring]] to 425[[ring]]C at +/-2[[ring]] Torsion (Woods' F-Range). March 1970

143 KIM, C. S., A Fundamental Study of the Current Density Distribution in a Flowing Non-Equilibrium Plasma. Sept. 1969

144 ELSENAAR, A., A Numerical Model for a Combustion-Driven Spherical Implosion Wave. Oct. 1969

145 ELSENAAR, A., Microwave Measurements of Projectile Motion in the Barrel of the UTIAS Implosion Driven Hypervelocity Launcher. Sept. 1969

146 RIBNER, H. S., Eddy Mach Wave Noise from a Simplified Model of a Supersonic Mixing Layer. Oct. 1969

147 DAWSON, V.C.D., WASER, R. A. and OAKES, D. O., The MK II UTIAS Implosion-Driven Hypervelocity Launcher Design Analysis. March 1970

148 LAW, C. K. and BRISTOW, M., Tables of Normal Shock Wave Properties for Oxygen and Nitrogen in Dissociation Equilibrium. Dec. 1969

149 KONDO, Y. and LAW, C. K., Normal Shock Wave Properties in Dissociated Chlorine. July 1970

150 LAW, C. K., Diffraction of Strong Shock Waves by a Sharp Compressive Corner. July 1970

151 NGUYEN, P. K., A Practical Method for Optimum Transient Riddance in Damped Linear Systems. July 1970

152 UNPUBLISHED

153 LAM, C. K., Development of a Nozzle Beam Containing Atomic Oxygen. July 1970

154 MacPHERSON, A. K., A Preliminary Study of Spherical Detonation Wave Symmetry in Stoichiometric Hydrogen Oxygen Mixtures. Feb. 1970

155 UNPUBLISHED

156 UNPUBLISHED

157 EVANS, R. L., Calibration of a Condenser Microphone Micrometeoroid Sensor. Sept. 1970

158 LIN, S., Sonic Boom Analogue for Investigating Indoor Waves and Structural Response. Nov. 1970

159 HAMEL, D. R., Bonded Joints -- Increasing Fatigue Strength by Bevelling. Sept. 1970

160 NIRANJAN, V., HAMEL, D. R. and YANG, C. A., Static and Fatigue Strengths of FM-123-2 Adhesive in Double Strap Joints of Various Lengths of Overlap. April 1971

161 CHAN, S. K., CAPPELLI, G. and GRAF, W. O., Performance Trials of the Eight-Inch Diameter UTIAS Implosion Driven Hypervelocity Launchers MK II and MK III. April 1971

162 DAVIS, P. L., Feasibility Study of a Proposed Control System on a Hydrofoil Sailboat. March 1971

163 SISSON, A. E., Quantum Transition Calculations for Gas-Surface Interactions. April 1971

164 NIRANJAN, V., Bonded Structures and the Optimum Design of a Joint. July 1971

165 LAKE, R. and ALLEN, G., Trajectories of Rain Drops Through a Two-Dimensional Vertically Blown Jet in a Horizontal Wind. Nov. 1971

166 LASZLO, G. P., Trace Gas Analysis by Mobility Separation. Dec. 1971

167 FROSTELL, C. E., A Comparison of Pilot Describing Function Measurement Techniques. Oct. 1971

168 ONYEONWU, R. O., On the Effects of Wind and Temperature Gradients on Sonic Boom Corridors. Oct. 1971

169 DERZKO, N. A., Near-Free-Molecule Flow Calculations -- Monte Carlo Study of Skimmer Interactions. Oct. 1971

170 APPARAO, T.A.P.S., Design and Installation of a Wind Tunnel Fan. Dec. 1971

171 ALLEN, G.A.S., Experimental Investigation of an Air Curtain for Protection of an Outdoor Power Installation from Salt Spray. Aug. 1971

172 MASTORIS, S., The Three-Dimensional Quadrupole Mass Spectrometer. Jan. 1972

173 BERG, A., Longitudinal Splitting of a Wind Tunnel Moving Ground Belt and Its Effect on a Jet Flap Model. Jan. 1972

174 RIBNER, H. S., Supersonic Turns Without Superbooms. Feb. 1972

175 WETTLAUFER, D. E., An Interferometric Determination of the Specific Refractivities of the Nitrogen and Oxygen Atoms. Feb. 1972

176 DREWELL, N. H., The Effect of Preview on Pilot Describing Functions in a Simple Tracking Task. May 1972

177 JOHNSTON, G. W., V/STOL Community Annoyance Due to Noise Proposed Indices and Levels (Toronto-York Transportation Committee). March 1972

178 WATSON, B. L., The Effect of Secondary Tasks on Pilot Describing Functions in a Compensatory Tracking Task. June 1972

179 LIPS, K. W., An Unstable Steering Task with a Sonic-Boom Disturbance. Sept. 1972

180 CAROTHERS, R., Initial Calibration and Physiological Response Data for the Travelling-Wave Sonic-Boom Simulator. Aug. 1972

181 HARTING, A., The UTIAS Precipitation Wind Tunnel. Sept. 1972

182 LAKE, R. and ETKIN, B., Experimental Simulation of the Interaction of Wind Driven Precipitation with an Annular Air Curtain Dome. March 1973

183 MOHR, D. J., Aircraft Transition Algorithm for Reference to the North Atlantic Air Traffic Control System. Jan. 1973

184 DAVIES, W.E.R., Velocity Measurements in Bubbly Two-Phase Flows Using Laser Doppler Anemometry (Part I). Oct. 1971

185 DAVIES, W.E.R. and UNGER, J., Velocity Measurements in Bubbly Two-Phase Flows Using Laser Doppler Anemometry (Part II). Dec. 1972

186 TEUNISSEN, H. W. and SCHUYLER, G., Design and Calibration of the UTIAS Boundary Layer Simulation Wind Tunnel. Dec. 1974

187 BRIMELOW, P. I., An Interferometric Investigation of Shock Structure and Its Induced Shock-Tube Boundary Layer in Ionized Argon. July 1974

188 NOWAKIWSKY, O. V., Effects of Sonic Boom on Automobile-Driver Behaviour. May 1974

189 BAND, D., A Preliminary Study of the Feasibility of an Air Cushion Vehicle Simulation. April 1974

190 ELLIS, N. D., RUSHWALD, I. B. and RIBNER, H. S., Development of a Portable Sonic Boom Simulator for Field Use. July 1974

191 LEIGH, B. R., Lifetime Concept of Plaster Panels Subjected to Sonic Boom. June 1974

192 HAASZ, A. A., ETKIN, B., LAKE, R. T. and GOERING, P.L.E., Laboratory Simulation of an Air-Curtain Roof for the Ontario Science Centre. Feb. 1975

193 NOSSEIR, N.S.M., Correlation of Jet Noise Data in Terms of a Self Noise-Shear Noise Model. Jan. 1975

194 KELSALL, J. T., Suppression of Refraction in Jet Noise by Cooling. May 1975

195 LIU, W. S., Integral Method of Solution for Compressible Laminar Boundary Layers and Applications. Dec. 1975

196 SHARMA, S. P., Production of Diamonds from Graphite Using Explosive-Driven Implosions. Dec. 1975

197 FRASER, A. J., Development and Testing of a Fixed-Base Hovercraft Simulator. Dec. 1975

198 ABDEL-RAHMAN, T., Influence of Structural Flexibility on a Single-Axis Linear Attitude Controller. Feb. 1976

199 MALICH, G., Effects of Structural Flexibility on a Reaction Jet Satellite Attitude Control System. Dec. 1975

200 SINCARSIN, G., Dynamics of the CTS Development Model Solar Array. May 1976

201 ROIG, R. A., Equilibrium Composition Data for Combustible Stoichiometric Mixtures of Hydrogen-Oxygen (Water). April 1976

202 JANKOVIC, M. S., Lateral Vibrations of an Extending Rod. June 1976

203 DAVIES, W.E.R. and DE LEEUW, J. H., Velocity Measurements on the Aerodynamic Wake of a Hovercraft Using Laser Doppler Anemometry. June 1976

204 SULLIVAN, P. A. and PARRAVANO, G. J., Theoretical Analysis of a Loop Type Flexible Skirt Air Cushion. June 1977

205 DELAURIER, J. D., An Investigation of the Effect of Ballonet Motions on Tethered-Aerostat Longitudinal Dynamic Stability. May 1977

206 SINCARSIN, G. B., Dynamical Model for the CTS Development Model Solar Array Under the Influence of Gravity. July 1977

207 WAHBA, N. N., Pressures Inside a Room Subjected to Sonic Boom. May 1977

208 BEN-DOR, G. and WHITTEN, B. T., Interferometric Technique and Data Evaluation Methods for the UTIAS 10 cm x 18 cm Hypervelocity Shock Tube. March 1979

209 VASUDEVAN, B., Pressure Measurements at the Focus of Combustion-Driven Implosions. April 1977

210 SHINDMAN, H. D., The Evaluation of a Fixed-Base Hovercraft Simulator. May 1977

211 HINCHEY, M. J. and SULLIVAN, P. A., Duct Effects on the Dynamic Fan Characteristics of Air Cushion Systems. June 1977

212 TANG, F. C., Effects of Impurities on Shock Wave Stability and Structures in Ionizing Monatomic Gases. Nov. 1977

213 FRENCH, J. B., REID, N. M. and BUCKLEY, J. A., The Real-Time Detection of Trinitrotoluene (TNT) in Ambient Air Using the TAGA System. Dec. 1977

214 GOLLA, D. F., Linear State Feedback Control of Rigid-Link Manipulators. May 1979

215 NIEDZWIECKI, A. and RIBNER, H. S., Subjective Loudness of Sonic-Boom: N-Wave and Minimized (`Low-Boom') Signatures. Nov. 1977

216 BEAULIEU, G., The Effects of Wind Shear on Aircraft Flight Path and Methods for Remote Sensing and Reporting of Wind Shear at Airports. Feb. 1978

217 FUJII, Hironori, Review on Strapdown System (Kinematics, Alignment and State Estimation). March 1978

218 RIBNER, H. S., A Transonic Propeller of Triangular Plan Form (An Extension). May 1978

219 HAASZ, A. A. and RAIMONDO, S., Preliminary Wind Tunnel Simulation Study of Snow Collection Gauges. May 1979

220 SOLOWKA, E. N., The Effect of a Predictive Wind Shear Chart on Pilot Landing Performance. April 1980

221 HARTWELL, E. G., Application of On-Line Computer Techniques to Measurement and Control in a Multiple-Jet Wind Tunnel. May 1980

222 BUCHANAN, W. L., An Experimental Study of Time-Dependent Instabilities of Planar Shock Waves in Ionizing Argon. Aug. 1980

223 CAMPBELL, J. L., Attitude Estimation for a Bias-Momentum Geosynchronous Satellite Using an Adaptive Observer. March 1983

224 CHODAS, P., Application of the Extended Kalman Filter to Several Formulations of Orbit Determination. Aug. 1981

225 WONG, S. K., A Study of the Characteristics of an Atmospheric Pressure Microwave-Induced Argon Plasma. May 1980

226 FAIRGRIEVE, J. D. and DELAURIER, J. D., Propulsive Performance of Two-Dimensional Thin Airfoils Undergoing Large-Amplitude Pitch and Plunge Oscillations. July 1982

227 VON FLOTOW, A. H. and ETKIN, B., Performance of the University of Toronto Infrasizer MK III as a Monosizer and Multi-Cut Classifier. Dec. 1980

228 KEITH, S. E. and SCHOLAERT, H.S.B., A Study of the Performance of an Olson-Type Active Noise Controller and the Possibility of the Reduction of Cabin Noise. March 1981

229 HOLST-JENSEN, O., An Experimental Investigation of Rise Times of Very Weak Shock Waves. March 1981

230 KOTASEK, V., Negative Ion/Molecule Reactions in a Negative Corona Discharge. April 1981

231 ANDO, S., Pseudo-Stationary Oblique Shock Wave Reflection in Carbon Dioxide -- Domains and Boundaries. April 1981

232 HU, Z., Jet Response to Pure Tone Excitation. Jan. 1982

233 SAGIE, D. and GLASS, I. I., Explosive-Driven Hemispherical Implosions for Generating Fusion Plasmas. March 1982

234 HINCHEY, M. J., SULLIVAN, P. A. and DUPUIS, A., Wave Propagation Effects on the Heave Dynamics of Large Air Cushion Platforms. Aug. 1982

235 SHENG, Y. and SISLIAN, J. P., Interaction of Oblique Shock and Detonation Waves. Feb. 1982

236 HINCHEY, M. J., Heave Stability of Air Cushion Vehicles Hovering Over Deep Water. Aug. 1982

237 WONG, R.L.M. and HU, Zhangwei, The Influence of Fresnel Number and Secondary Geometric Parameters on the Diffracted Field of Planar Lamina. May 1982

238 MacKENZIE, R. B., A Piloted Flight Simulator Study of Conflict of Interest Wind Modelling Techniques. Nov. 1982

239 GOTTLIEB, J. J., SAITO, T. and ZHANG, K. Y., Numerical Prediction of Blast-Wave Flows Outside and Inside a Power House of a Nuclear-Power Generating Station. April 1985

240 NAHON, M. A., A Study of Lateral Flight Path Perturbations of STOL Aircraft in the Planetary Boundary Layer. June 1983

241 BRESSERS, A.J.N., Pressures Inside Coupled Rooms Subject to Sonic Boom. Feb. 1983

242 SINCARSIN, G. B., Geostationary Orbital Estimation Using a Kalman Filter. Aug. 1986

243 HUGHES, P. C. and GOLLA, D. F., Stability Diagrams for a Rigid Gyrostat in a Circular Orbit. May 1984

244 SADEK, H.S.I. and GOTTLIEB, J. J., Initial Decay of Flow Properties of Planar, Cylindrical and Spherical Blast Waves. Oct. 1983

245 ZINGG, D. W., An Approach to the Design of Airfoils with High Lift to Drag Ratios. April 1983

246 LIU, Z.-Q., A Study of Washout Filters for a Simulator Motion Base. Dec. 1983

247 BYRNE, J. E., Design of a Lateral Ride Comfort Control System for STOL Aircraft. Dec. 1983

248 WONG, C. H., An Experimental and Numerical Study of Weak Spherical N-Waves Produced by Exploding Wires. Jan. 1984

249 SHEN, F., A Quantitative Comparison of Active and Passive Damping for Large Space Structures. Feb. 1985

250 UNPUBLISHED

251 LAU, S.C.M. and GOTTLIEB, J. J., Numerical Reconstruction of Part of an Actual Blast-Wave Flow Field to Agree with Available Experimental Data. Aug. 1984

252 HUGHES, P. C., Space Structure Vibration Modes: How Many Exist? Which Ones are Important? April 1984

253 HU, J.T.C., Pseudo-Stationary Oblique-Shock-Wave Reflections in a Polyatomic Gas -- Sulfur Hexafluoride. Jan. 1985

254 LANOUETTE, A., Design and Analysis of a Longitudinal Ride Comfort Control System for a Short Take-Off and Landing (STOL) Aircraft. April 1984

255 MURTY, H. S. and GOTTLIEB, J. J., Analytical and Numerical Study of the Flow in a Shock Tube with an Area Change at the Diaphragm Section. May 1984

256 WHEELER, J., An Interferometric Investigation of the Regular to Mach Reflection Transition Boundary in Pseudostationary Flow in Air. April 1986

257 SHENG, Y. and SISLIAN, J. P., A Model of a Hypersonic Two-Dimensional Oblique Detonation Wave Ramjet. July 1985

258 ANDERSON, D. S. and GOTTLIEB, J. J., On Random Numbers for the Random-Choice Method. Sept. 1987

259 GROTH, C.P.T., Quick Reproduction of Blast-Wave Flow-Field Properties of Nuclear, TNT and ANFO Explosions. April 1986

260 RIBNER, H. S., Spectra of Noise and Amplified Turbulence Emanating from Shock-Turbulence Interaction: Two Scenarios (pre-shock vs. axisymmetry). March 1986

261 GRANT, P. R., Motion Characteristics of the UTIAS Flight Research Simulator Motion-Base. July 1986

262 DIETZ, P.R.W., Determination of the Efficacy of Using Accelerometers as Sensors for Third Generation Satellites. Dec. 1986

263 CZERWINSKI, W., DESCHAMBAULT, R. L. and LOCK, G. D., Design of a Dusty-Gas Shock-Tube Facility with Preliminary Experimental Results. May 1987

264 PIPERNI, P., A Complete Linearized Theory for the Analysis and Design of Two-Dimensional Hydrofoils Near a Free Surface. Oct. 1987

265 CHEUNG, R.S.W., Numerical Prediction of Propeller Performance by Vortex Lattice Method. Nov. 1987

266 GROTH, C.P.T., GOTTLIEB, J. J. and BOURGET, C., Ideal-Viscoelastic Extrusion Model with Application to Deforming Pistons in Light-Gas Guns. Nov. 1987

267 URBANOWICZ, J. T., Pseudo-Stationary Oblique-Shock-Wave Reflections in Low Gamma Gases -- Isobutane and Sulphur Hexafluoride. Feb. 1988

268 PAIGE, A. B., An Experimental Study of a Laminar Wall-Jet in the Presence of a Uniform External Flow. March 1988

269 KACA, J., An Interferometric Investigation of the Diffraction of a Planar Shock Wave Over a Semicircular Cylinder. Sept. 1988

270 SMITH, D. S., Flow Characteristics About a Trailing Edge. March 1989

271 FOSTER, S. P., Ideal Efficiency of Propellers: Theodorsen Restudied with Recomputed and Simplified Charts. Foreword and Appendix Segments by H. S. Ribner. Nov. 1990

272 KIRDEIKIS, J., Evaluation of Nonlinear Motion-Drive Algorithms for Flight Simulators. June 1989

273 ROMANO, R. A., The Evaluation of the Electrogastrogram for Use in Simulator Sickness Studies. Feb. 1990

274 CHEN, L. C., A Unique Method of Determining the Elastic and Engineering Constants of Unidirectional Fibre-Reinforced Composite Plates Using Ultrasound. Nov. 1990

275 SISLIAN, J. P., HE, Z., and DESCHAMBAULT, R. L., An Experimental Study of Hypersonic Flow Development in a Pipe. Aug. 1991

276 SHARF, I., and D'ELEUTERIO, G. M. T., An Iterative Approach to Multibody Simulation Dynamics Suitable for Parallel Implementation. Sept. 1994