PKK Library Search for 'se,phr:"Institute For Aerospace Studies"'

AN EJECTOR-DRIVEN WIND TUNNEL FOR THE GENERATION OF TURBULENT FLOWS WITH ARBITRARY MEAN VELOCITY PROFILE.

By Teunissen, H.W.. , Bound With : Ias Ut 131-137

Place Hold on AN EJECTOR-DRIVEN WIND TUNNEL FOR THE GENERATION OF TURBULENT FLOWS WITH ARBITRARY MEAN VELOCITY PROFILE.

ASSESSMENT AND DEVELOPMENT OF METHODS OF ACOUSTIC PERFORMANCE PREDICTION FOR JET NOISE SUPPRESSORS

By Middleton, D.. , Bound With: Ias Ut 131-137

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DISCUSSION OF APPROXIMATE THEORIES FOR INVISCID HYPERSONIC FLOW ON CONCAVE SURFACES

By Sullivan,P. A.. University Of Toronto, Toronto 1970 . 20 , Bound With: Ias-Ut-140-145

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EFFECT OF HIGH INTENSITY TURBULENCE ON THE AERODYNAMICS OF A RIGID CIRCULAR CYLINDER AT SUBCRITICAL REYNOLDS NUMBER

By Surry,D.. University Of Toronto, Toronto 1969 . 44 , Bound With: Ias-Ut-140-145

Place Hold on EFFECT OF HIGH INTENSITY TURBULENCE ON THE AERODYNAMICS OF A RIGID CIRCULAR CYLINDER AT SUBCRITICAL REYNOLDS NUMBER

CRITICAL EVALUATION OF THE METASTABLE TIME OF FLIGHT TECHNIQUE FOR OBTAINING MOLECULAR VELOCITY DISTRIBUTION

By Locke,J. W.. University Of Toronto, Toronto 1969 . 46 , Bound With: Ias-Ut-140-145

Place Hold on CRITICAL EVALUATION OF THE METASTABLE TIME OF FLIGHT TECHNIQUE FOR OBTAINING MOLECULAR VELOCITY DISTRIBUTION

ON THE MODALITY OF FATIGUE ENDURANCE DISTRIBUTIONS IN OFHC COPPER

By Korbacher,G. K.. University Of Toronto, Toronto 1970 . 23 , Bound With: Ias-Ut-140-145

Place Hold on ON THE MODALITY OF FATIGUE ENDURANCE DISTRIBUTIONS IN OFHC COPPER

EXPERIMENTAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF A MODEL OF AN AIR CUSHION VEHICLE IN HOVERING FLIGHT

By Gowans,B. W.. University Of Toronto, Toronto 1964 . 16 , Bound With: Ias-Ut-73-79

Place Hold on EXPERIMENTAL STUDY OF THE AERODYNAMIC CHARACTERISTICS OF A MODEL OF AN AIR CUSHION VEHICLE IN HOVERING FLIGHT

CHARACTERISTICS OF A RECTANGULAR WING WITH APERIPHERAL JET IN GROUND EFFECT,PART III

By Surry,D.. University Of Toronto, Toronto 1964 . 25 , Bound With: Ias-Ut-73-79

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COANDA EFFECT AT DEFLECTION SURFACES WIDELY SEPARATED FRON THE JET NOZZLE

By Benner,S. D.. University Of Toronto, Toronto 1965 . 21 , Bound With: Ias Ut-73-79

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EXPERIMENTAL INVESTIGATION INTO THE SHAPE OF THROUST AUGMENTING SURFACES IN CONJUNCTION WITH COANDA-DEFLECTED JET SHEETS(PART II)

By Mehus,T.. University Of Toronto, Toronto 1965 . 30 , Bound With: Ias-Ut-73-79

Place Hold on EXPERIMENTAL INVESTIGATION INTO THE SHAPE OF THROUST AUGMENTING SURFACES IN CONJUNCTION WITH COANDA-DEFLECTED JET SHEETS(PART II)

LOW ENERGY NITROGEN ION BEAM

By Prince,R. H.. University Of Toronto, Toronto 1965 . 36 , Bound With: Ias-Ut-80-85

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APPLICATION OF A JET PUMP AND COANDA SURFACE TO VENTILATION OF A HIGHWAY TUNNEL

By Nishimura,Y.. University Of Toronto, Toronto 1965 . 33 , Bound With: Ias -Ut-80-85

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PRELIMINARY ONE-DIMENSIONAL INVESTIGATION OF THE INITIATION OF LOW-DENSITY PETN

By Makomaski,A. H.. University Of Toronto, Toronto 1965 . 24 , Bound With: Ias-Ut-80-85

Place Hold on PRELIMINARY ONE-DIMENSIONAL INVESTIGATION OF THE INITIATION OF LOW-DENSITY PETN

THERMODYNAMIC AND COMPOSITION DATA FOR CONSTANT-VOLUME COMBUSTION OF STOICHIOMETRIC MIXTURES OF HYDROGEN-OXYGEN DILUTED WITH HELIUM OR HYDROGEN

By Benoit,Andre. University Of Toronto, Toronto 1964 . 18 , Bound With: Ias-Ut-80-85

Place Hold on THERMODYNAMIC AND COMPOSITION DATA FOR CONSTANT-VOLUME COMBUSTION OF STOICHIOMETRIC MIXTURES OF HYDROGEN-OXYGEN DILUTED WITH HELIUM OR HYDROGEN

ON THE LATERAL INSTABITIES OF AIRCRAFT DUE TO PARAMETRIC EXCITATION

By Masak,M.. University Of Toronto, Toronto 1965 . 38 , Bound With: Ias,Ut-86-92

Place Hold on ON THE LATERAL INSTABITIES OF AIRCRAFT DUE TO PARAMETRIC EXCITATION

TURBULENCE PROPE UTILIZING AERODYNAMIC LIFT

By Siddon,T. E.. University Of Toronto, Toronto 1965 . 15 , Bound With: Ias ,Ut-86-92

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EXPERIMENTAL INVESTIGATION OF THE CHARACTERISTICS OF FLOW ABOUT CURVED CIRCULAR CYLINDERS

By Surry,Jean. University Of Toronto,Toronto 1965 . 24 , Bound With: Ias-Ut-86-92

Place Hold on EXPERIMENTAL INVESTIGATION OF THE CHARACTERISTICS OF FLOW ABOUT CURVED CIRCULAR CYLINDERS

DETERMINATION OF DIAPHRAGM OPENINGTIMES AND USE OF DIAPHRAGM PARTICLE TRAPS IN A HYPERSONIC SHOCK TUBE

By Drewry,J. E.. University Of Toronto, Toronto 1965 . 18 , Bound With: Ias,Ut-86-92

Place Hold on DETERMINATION OF DIAPHRAGM OPENINGTIMES AND USE OF DIAPHRAGM PARTICLE TRAPS IN A HYPERSONIC SHOCK TUBE

FLOW OF LOW DENSITY AIR OVER A HEATED FLAT PLATE AT MACH NO.0.5

By Gordon,S. A.. University Of Toronto, Toronto 1964 . 60 , Bound With: Ias,Ut-86-92

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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%

By Hyghes,P. C.. University Of Toronto,Toronto 1965 . 21 , Bound With: Ias,Ut-86-92

Place Hold on 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%

STUDY OF THE INTERACTION OF A LANINAR HYPERSONIC BOUNDARY LAYER WITH ACORNER EXPANSION WAVE

By Lo,A. K.. University Of Toronto, Toronto 1970 . 31 , Bound With: Ias-Ut-156-161

Place Hold on STUDY OF THE INTERACTION OF A LANINAR HYPERSONIC BOUNDARY LAYER WITH ACORNER EXPANSION WAVE

EXPERIMENTAL DETERMINATION OF THE POLARIZABILITY FOR SINGLY LONIZED ARGON

By Bristow,M.P.F.. University Of Toronto, Toronto 1971 . 49 , Bound With: Ias-Ut-156-161

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EXPERIMENATAL INVESTIGATION OF A NONEQUILIBRIUM CORNER-EXPANSION FLOW OF LONIZED ARGON

By Igra,O.. University Of Toronto, Toronto 1970 . 33 , Bound With: Ias-Ut-156-161

Place Hold on EXPERIMENATAL INVESTIGATION OF A NONEQUILIBRIUM CORNER-EXPANSION FLOW OF LONIZED ARGON

SUPERSONIC TURNS WITHOUT SUPERBOOMS

By Ribner,H. S.. Institute For Aerospace Studies, Toronto 1972 . 7 , Bound With: Ias Ut 174-180

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INTERFEROMETRIC DETERMINATION OF THE SPECIFIC REFRACTIVITIES OF THE NITROGEN AND OXYGEN ATOMS

By Wettlaufer,Dale E.. Institute For Aerospace Studies, Toronto 1972 . 15 , Bound With: Ias Ut 174-180

Place Hold on INTERFEROMETRIC DETERMINATION OF THE SPECIFIC REFRACTIVITIES OF THE NITROGEN AND OXYGEN ATOMS

EFFECT OF PRIVIEW ON PILOT DESCRIBING FUNCTIONS IN A SIMPLE TRACKING TASK

By Drewell,N. S.. Institute For Aerospace Studies, Toronto 1972 . 12 , Bound With: Ias Ut 174-180

Place Hold on EFFECT OF PRIVIEW ON PILOT DESCRIBING FUNCTIONS IN A SIMPLE TRACKING TASK

V STOL COMMUNITY ANNOYANCE DUE TO NOISE PROPOSED INDICES AND LEVELS FOR TORONTO-YORK TRANSPORTATION COMMITTEE

By Johnston,G. W.. Institute For Aerospace Studies, Toronto 1972 . 20 , Bound With: Ias Ut 174-180

Place Hold on V STOL COMMUNITY ANNOYANCE DUE TO NOISE PROPOSED INDICES AND LEVELS FOR TORONTO-YORK TRANSPORTATION COMMITTEE

EFFECT OF SECONDARY TASKS ON PILOT DESCRIBING FUNCTIONS IN A COMPENSATORY TRACKING TASK

By Watson,B. L.. Institute For Aerospace Studies, Toronto 1972 . 15 , Bound With: Ias Ut 174-180

Place Hold on EFFECT OF SECONDARY TASKS ON PILOT DESCRIBING FUNCTIONS IN A COMPENSATORY TRACKING TASK

SHOCK WAVE STRUCTURE IN GAS MIXTURES AND PLASMAS

By Sinclair,S.R.M.. University Of Toronto, Toronto 1968 . 51 , Bound With : Ias Ut 130-134

Place Hold on SHOCK WAVE STRUCTURE IN GAS MIXTURES AND PLASMAS

STUDY OF THE INITIAL IONIZATION PROCESS IN A STRONG SHOCK WAVE

By Belozerov,A.. University Of Toronto, Toronto 1968 . 37 , Bound With : Ias Ut 130-134

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SCATTERING OF HIGH ENERGY ARGON ATOMS FROM A WELL CHARACTERIZED (100) TUNGSTEN SURFACE

By O'Keefe,D. R.. University Of Toronto, Toronto 1968 . 39 , Bound With : Ias Ut 130-134

Place Hold on SCATTERING OF HIGH ENERGY ARGON ATOMS FROM A WELL CHARACTERIZED (100) TUNGSTEN SURFACE

INTERACTION OF LOW ENERGY ATMOSPHERIC IONS WITH CONTROLLED SURFACES

By Prince,R. H.. University Of Toronto, Toronto 1968 . 52 , Bound With : Ias Ut 130-134

Place Hold on INTERACTION OF LOW ENERGY ATMOSPHERIC IONS WITH CONTROLLED SURFACES

THEORY OF GAS-SURFACE INTERACTIONS AT SATELLITE VELOCITIES

By Jackson,D. P.. University Of Toronto, Toronto 1968 . 76 , Bound With : Ias Ut 130-134

Place Hold on THEORY OF GAS-SURFACE INTERACTIONS AT SATELLITE VELOCITIES

REFRACTION OF SOUND BY JET FLOW AND JET TEMPERATURE II

By Grande,E.. University Of Toronto, Toronto 1967 . 15 , Bound With:Ias Ut 110-116

Place Hold on REFRACTION OF SOUND BY JET FLOW AND JET TEMPERATURE II

ATTEMPT TO CORRELATE BIMODAL FATIGUE ENDURANCE DISTRIBUTIONS IN OFHC COPPER WITH WOOD'S H,F AND S RANGES

By Muggeridge,D. B.. University Of Toronto, Toronto 1967 . 12 , Bound With:Ias Ut 110-116

Place Hold on ATTEMPT TO CORRELATE BIMODAL FATIGUE ENDURANCE DISTRIBUTIONS IN OFHC COPPER WITH WOOD'S H,F AND S RANGES

STATISTICAL ASPECTS OF COEXISTING FATIGUE FAILURE MECHANISMS IN OFHC COPPER

By Haagensen,P. J.. University Of Toronto, Toronto 1967 . 16 , Bound With:Ias Ut 110-116

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IMPLOSION DRIVEN HYPERVELOCITY LAUNCHER PERFORMANC USING GASEOUS DETONATION WAVES

By Watson,J. D.. University Of Toronto, Toronto 1967 . 26 , Bound With:Ias Ut 110-116

Place Hold on IMPLOSION DRIVEN HYPERVELOCITY LAUNCHER PERFORMANC USING GASEOUS DETONATION WAVES

DISCONTINUOUS SOLUTIONS FOR NONEQUILIBRIUM SUPERSONIC FLOWS

By Tirumalesa,Duvvuri. University Of Toronto, Toronto 1967 . 18 , Bound With:Ias Ut 110-116

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RESPONSE OF A CYLINDRICAL STRUCTURE TO A TURBULENT FLOW FIELD AT SUBCRITICAL REYNOLDS NUMBER

By Campbell,A. C.. University Of Toronto, Toronto 1967 . 14 , Bound With:Ias Ut 110-116

Place Hold on RESPONSE OF A CYLINDRICAL STRUCTURE TO A TURBULENT FLOW FIELD AT SUBCRITICAL REYNOLDS NUMBER

EFFECTS OF SPECIMEN GRAIN SIZE AND ENVIRONMENT ON THE FATIGUE LIFE OF OFHC COPPER

By Knapp,W.. University Of Toronto, Toronto 1968 . 10 , Bound With:Ias Ut-123-130

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SPINNING HOT-WIRE ANEMOMETER FOR SIMULTANEOUS MEASUREMENT OF U,VAND W

By Mcleod,M. G.. University Of Toronto, Toronto 1967 . 17 , Bound With:Ias Ut-123-130

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EXPERIMENTAL INVESTIGATION OF SHOCK-WAVE DIFFRACTION OVER COMPRESSION AND EXPANSION CORNERS

By Weynants,R. R.. University Of Toronto, Toronto 1967 . 20 , Bound With:Ias Ut-123-130

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GEOMETRICAL PROPERTIES IN STATE SPACE OF LINEAR DIFFERENTIAL EQUATIONS WITH PERIODIC COEFFICIENTS

By Hughes,P. C.. University Of Toronto, Toronto 1968 . 24 , Bound With:Ias Ut-123-130

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EQUILIBRIUM THERMODYNAMIC DATA FOR THE H2-O2-HE SYSTEM

By Benoit,Andre. University Of Toronto, Toronto 1968 . 5 , Bound With:Ias Ut-123-130

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ON THE INTERACTION OF A LAMINAR HYPERSONIC BOUNDARY LAYER AND A CORNER EXPANSION WAVE

By Sullivan,Philip A.. University Of Toronto, Toronto 1968 . 15 , Bound With:Ias Ut-123-130

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OPTIMIZATION STUDY OF THE UTIAS IMPLOSION-DRIVEN HYPERVELOCITY LAUNCHER MK II

By Flagg,Robert F.. U.S. Environmental Proetction Agency, Washington 1968 . 20 , Bound With:Ias Ut-123-130

Place Hold on OPTIMIZATION STUDY OF THE UTIAS IMPLOSION-DRIVEN HYPERVELOCITY LAUNCHER MK II

PROPERTIES OF THE TURBULENCE IN THE TRANSITION REGION OF A ROUND JET

By Nayar,B. M., Siddon,T. E.. University Of Toronto, Toronto 1969 . 16 , Bound With:Ias Ut 131-137

Place Hold on PROPERTIES OF THE TURBULENCE IN THE TRANSITION REGION OF A ROUND JET

SPHERICAL ELASTIC-PLASTIC WAVES IN SOLID MEDIA

By Garg,Subodh K.. University Of Toronto, Toronto 1969 . 22 , Bound With:Ias Ut 131-137

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ON THE USE OF FLEXIBLE STRINGS IN GRAVITY-GRADIENT STABILIZATION

By Garg,S. C.. University Of Toronto, Toronto 1969 . 33 , Bound With:Ias Ut 131-137

Place Hold on ON THE USE OF FLEXIBLE STRINGS IN GRAVITY-GRADIENT STABILIZATION

PRELIMINARY INVESTIGATION OF A UT IAS IMPLOSION-DRIVEN SHOCK TUBE

By Poinssot,J. C.. University Of Toronto, Toronto 1969 . 21 , Bound With:Ias Ut 131-137

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SPIN DECAY OF A CLASS OF SATELLITES CAUSED BY SOLAR RADIATION

By Cherchas,D. B.. University Of Toronto, Toronto 1969 . 20 , Bound With:Ias Ut-131-137

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USE OF SELF CALIBRATING CATALYTIC PROBES TO MEASURE FREE-STREAM ATOM CONCENTRATION IN A HYPERSONIC FLOW

By Reddy,N. M.. University Of Toronto, Toronto 1966 . 43 , Bound With: Ias Ut 121-124

Place Hold on USE OF SELF CALIBRATING CATALYTIC PROBES TO MEASURE FREE-STREAM ATOM CONCENTRATION IN A HYPERSONIC FLOW

SUPERSONIC FLOW OF INVISCID COMPRESSIBLE PLASMAS WITH A FINITE TENSOR CONDUCTIVITY IN THE PRESENCE OF AN EXTERNAL MAGNETIC FIELD

By Shih,Lung Yu. University Of Toronto, Toronto 1966 . 43 , Bound With: Ias Ut 121-124

Place Hold on SUPERSONIC FLOW OF INVISCID COMPRESSIBLE PLASMAS WITH A FINITE TENSOR CONDUCTIVITY IN THE PRESENCE OF AN EXTERNAL MAGNETIC FIELD

NOZZLE FLOWS WITH COUPLED VIBRATIONAL AND DISSOCIATIONAL NONEQUILIBRIUM

By Tirumalesa,Duvvuri. University Of Toronto, Toronto 1967 . 118 , Bound With: Ias Ut 121-130

Place Hold on NOZZLE FLOWS WITH COUPLED VIBRATIONAL AND DISSOCIATIONAL NONEQUILIBRIUM

EXPERIMENTAL INMESTIGATION OF NONLIBRIUM CORNER EXPANSION FLOWS OF DISSOCIATED OXYGEN

By Drewry,J. E.. University Of Toronto, Toronto 1967 . 33 , Bound With: Ias Ut 121-124

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UNSTABLE STEERING TASK WITH A SONIC BOOM DISTRUBANCE

By Lips,K. W.. University Of Toronto, Toronto 1972 . 14 , Bound With: Ias Ut 174-180

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INITIAL CALIBRATION AND PHYSIOLOGICAL RESPONE DATA FOR THE TRAVELLING-WAVE SONIC-BOOM SIMULATOR

By Corothers,Richard. University Of Toronto, Toronto 1972 . 19 , Bound With: Ias Ut-174-180

Place Hold on INITIAL CALIBRATION AND PHYSIOLOGICAL RESPONE DATA FOR THE TRAVELLING-WAVE SONIC-BOOM SIMULATOR