University of Toronto. Institute for Aerospace Studies
Institute for Aerospace Studies (Toronto)
Institut d'études aérospatiales de l'Université de Toronto institut de recherche au Canada
VIAF ID: 153551598 (Corporate)
Permalink: http://viaf.org/viaf/153551598
Preferred Forms
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110 2 _
‡a
Institut d'études aérospatiales de l'Université de Toronto
‡c
institut de recherche au Canada
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110 2 _ ‡a Institute for Aerospace Studies (Toronto)
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110 2 _
‡a
University of Toronto
‡b
Institute for Aerospace Studies
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110 2 _ ‡a University of Toronto ‡b Institute for Aerospace Studies
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110 2 _
‡a
University of Toronto
‡b
Institute for Aerospace Studies
-
110 2 _
‡a
University of Toronto. Institute for Aerospace Studies
-
110 2 _ ‡a University of Toronto. ‡b Institute for Aerospace Studies
-
110 2 _
‡a
University of Toronto.
‡b
Institute for Aerospace Studies
-
110 2 _ ‡a University of Toronto. ‡b Institute for Aerospace Studies
-
110 2 _ ‡a University of Toronto. ‡b Institute for Aerospace Studies
4xx's: Alternate Name Forms (18)
5xx's: Related Names (7)
- 510 2 _
‡a
Institute of Aerophysics Toronto
- 551 _ _
‡a
Toronto
‡4
orta
‡4
http://d-nb.info/standards/elementset/gnd#placeOfBusiness
- 510 2 _
‡a
University Toronto
- 510 2 _
‡a
University of Toronto.
‡b
Institute of Aerophysics
- 510 2 _
‡a
University of Toronto
‡b
Institute of Aerophysics
- 510 2 _
‡a
University of Toronto
‡b
Institute of Aerophysics
‡4
vorg
‡4
http://d-nb.info/standards/elementset/gnd#precedingCorporateBody
‡e
Vorgaenger
- 510 2 _
‡a
University of Toronto
‡4
adue
‡4
http://d-nb.info/standards/elementset/gnd#hierarchicalSuperiorOfTheCorporateBody
‡e
Ueberordnung
Works
| Title | Sources |
|---|---|
| Aerodynamic noise; proceedings of AFOSR-UTIAS Symposium, held at Toronto, 20-21 May 1968. |
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| Geometrijski pristup generiranju ostvarivih konfiguracija robotskih manipulatora |
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| Inviscid on-design propulsive characteristics of hypersonic shock-induced combustion ramjets |
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| Measurements of turbulence inputs for V/STOL approach paths in a simulated planetary boundary layer |
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| Mechanics of composite materials : an introductory course |
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| The mini-oscillator technique : a finite element method for the modelling of linear viscoelastic structures |
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| Molecular beams for rarefied gasdynamic research |
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| Motion characteristics of the UTIAS Flight Research Simulator Motion-Base |
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| Near resonant vibration tests of an orbiting flexible spacecraft. |
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| Nonlinear aspects of transonic aeroelasticity |
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| Nonlinear scattering of ultrasound by bubbles : numerical and experimental investigations with application to their detection |
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| Normal reflection of a shock wave at a rigid wall in a dusty gas |
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| Numerical analysis of dusty supersonic flow past blunt axisymmetric bodies |
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| Numerical prediction of propeller performance by vortex lattice method |
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| Numerical study of unsteady flows in large air-driven blast simulators with single and multiple drivers |
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| The obstacle avoidance manoeuvre as performed in a tractor/semitrailer truck |
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| On the analysis of shell structures subjected to a blast environment : a finite element approach |
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| On the passage of a shock wave through a dusty-gas layer |
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| Optimization of laminated cylinders for buckling |
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| Orbital decay in a dynamic atmosphere |
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| The overpressure signature from a supersonic projectile |
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| Performance analysis of UTIAS implosion-driven hypervelocity launcher |
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| The plasma current multiplier |
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| Prediction of two-dimensional time-dependent gasdynamic flows for hypersonic studies |
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| Preliminary wind tunnel simulation study of snow collection gauges |
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| Pressures inside coupled rooms subjected to sonic boom |
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| Prog. rep. educ. res. |
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| Progress report, education and research |
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| Propulsive performance of two-dimensional thin airfoils undergoing large-amplitude pitch and plunge oscillations |
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| The race for unlimited energy |
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| Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flows |
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| Random-choice solutions for weak spherical shock-wave transitions of N-waves in air with vibrational excitation |
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| The real-time detection of trinitrotoluene (TNT) in ambient air using the Taga system. |
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| Regions and transitions of nonstationary oblique shock-wave diffractions in perfect and imperfect gases |
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| The response of a cylindrical structure to a turbulent flow field at subcritical Reynolds number |
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| Review of adaptive-grid techniques for solution of partial differential equations |
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| Review of the status of MHD power generation technology including suggestions for a Canadian MHD research program; |
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| Simulation of a blast wave in a shock tube by using perforated plates in the driver |
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| Simulation of the planetary boundary layer in a multiple-jet wind tunnel |
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| Some aspects of shock-wave research |
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| Sonic boom analogues for investigating indoor waves and structural response. |
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| Sonic line in nonequilibrium flows |
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| [Specific suggestions for a fusion insurance program] |
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| Spectra of noise and amplified turbulence emanating from shock-turbulence interaction : two scenarios |
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| Stability diagrams for a rigid gyrostat in a circular orbit |
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| Static and fatigue strength of FM-123-2 adhesive in double strap joints of various lengths of overlap |
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| STOL technology bibliography update : a study prepared for the Canadian Transport Commission, Systems Analysis Branch |
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| Studies of laser selective excitation of atoms |
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| Study of low-Z coatings for JET under exposure to electrons, laser radiation and atomic hydrogen |
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| Supersonic turns without superbooms |
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| Supression of refraction in jet noise by cooling. |
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| Survey of flows with nucleation and condensation |
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| Theoretical analysis of a loop type flexible skirt air cushion |
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| Theory of airfoil response in a gusty atmosphere. |
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| Tokamak plasma interaction with limiters |
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| Trace gas analysis by mobility separation |
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| Transition flow ion transport via integral Boltzmann equation |
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| Turbulent mixing in supersonic hightemperature exhaust jets, 1996: |
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| The turbulent wind and its effect on flight |
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| The universe and manned space flight |
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| University of Toronto Institute for Aerospace Studies report |
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| The UTIAS precipitation wind tunnel |
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| UTIAS report |
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| UTIAS Review No. 50. Over forty years of continuous research at UTIAS on nonstationary flows and shock waves. /By I.I. Glass. |
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| UTIAS review (Online) |
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| UTIAS technical note. |
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| The validation of a linear driver model |
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| Velocity measurements in bubbly two-phase flows using laser Doppler anemometry |
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| Wave propagation effects on the heave dynamics of large air cushion platforms |
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| Wind effects on structures |
|
