AIAA 85-1003-85-1050

Front Cover
American Institute of Aeronautics and Astronautics, 1985 - Aerothermodynamics

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Contents

Section 1
1
Section 2
9
Section 3
5

21 other sections not shown

Common terms and phrases

20th Thermophysics Conference AIAA AIAA Paper Aluminum analysis angle boundary conditions boundary layer calculated computed condenser configuration contour cross sections curves density diameter dimensionless dissociation droplet DSMC effects ELECTRON ENERGY enthalpy equation equilibrium experimental fibers Figure film boiling finite difference flight flow rate fluid flux tube Freon gage heat flux heat pipe heat rejection heat transfer coefficient heat-transfer heater Hypersonic Institute of Aeronautics insulation interface isothermal leading edge liquid Mach number mass flow rate measured molecule N₂ NASA nodes nonequilibrium nozzle nucleation Orbiter panel parameter payload pitot tube plate porous predicted pressure profiles radiative radiator rate coefficients rate constants region Reynolds number shock shown in Fig Shuttle simulation solution SOTRAN Space stagnation stream strong interaction subcooled surface temperature temperature distribution thermal conductivity thermocouple thickness tion two-phase vapor velocity vibrational excitation wall wind tunnel

Bibliographic information

TitleAIAA 85-1003-85-1050
Volume 3 of A Collection of Technical Papers: AIAA 20th Thermophysics Conference, June 19-21, 1985, Williamsburg, Virginia, American Institute of Aeronautics and Astronautics
ContributorAmerican Institute of Aeronautics and Astronautics
PublisherAmerican Institute of Aeronautics and Astronautics, 1985
Original fromPennsylvania State University
DigitizedMay 31, 2011
  
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