32nd Aerospace Sciences Meeting & Exhibit: 94-0670 - 94-0709

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American Institute of Aeronautics and Astronautics, 1994 - Aeronautics

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Contents

Section 1
11
Section 2
13
Section 3
11

28 other sections not shown

Common terms and phrases

AIAA AIAA Paper angle of attack atomic boundary layer bow shock calculated chemical coefficient collision combustion constant convection Delta Wing diameter diffusion flames downstream droplet dynamic effects eigenfunction electron elliptical jet energy enthalpy equations experimental experiments Figure flame speed flamelet flow field fluid freestream frequency fuel gravity grid heat release heat transfer helium increase initial injection injector interface laser liquid hydrogen Mach number mass fraction measurements microgravity mixing momentum thickness N₂ nacelle nitrogen nondimensional normal nozzle number density optical particles Phys plasma plot premixed Premixed Flames pressure profiles propagation radiation ratio reaction front reduced mechanism regime region Reynolds number rocket scale shear layer shown in Fig shows simulations slosh waves solution species spray strain rate streamwise structure suction dip supersonic surface temperature thermal tion transverse values velocity viscosity vortex vorticity Water Tunnel wind tunnel

Bibliographic information

Title32nd Aerospace Sciences Meeting & Exhibit: 94-0670 - 94-0709
Volume 21 of 32nd Aerospace Sciences Meeting & Exhibit: January 10-13, 1994, Reno, NV, American Institute of Aeronautics and Astronautics
ContributorAmerican Institute of Aeronautics and Astronautics
PublisherAmerican Institute of Aeronautics and Astronautics, 1994
Original fromPennsylvania State University
DigitizedJun 24, 2009
  
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