Aeroelastic instability caused by slender payloads.
Terminal shock-boundary layer interaction on slender cone-cylinder payloads at supersonic speeds and resulting flow separation
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Terminal shock-boundary layer interaction on slender cone-cylinder payloads at supersonic speeds and resulting flow separation
Integer relations method of determining inviscid shock layer flow and pressure distributions over blunt bodies
Three dimensional flow field induced ahead of shock wave by radiation from shock layer over blunt body, determining perturbation velocity potential
Asymptotic solutions of blunt body stagnation flows with nongray radiation emission and absorption, discussing radiation coupled shock layer flow fields
Transient flow field of sphere struck by normal shock wave noting wave diffraction and shock layer formation
Radiation properties of shock layer and nonequilibrium flows around probes entering earth, Mars, Venus and Jupiter atmosphere
Solution for shock layer energy equation with mass and convective heat transfer at hypersonic speed
Quantitative determination of reentry shock precursor absorption level and effect on surface radiation heating, calculating radiative flux from shock layer enthalpy distribution
Atmospheric gas composition effects on shock layer radiative heat transfer and heat shield response in Venus entry simulated by earth reentry
Nongray equilibrium radiative heat transfer in viscous radiating shock layer around blunt body entering high temperature nonisothermal carbon dioxide-nitrogen atmosphere
Shock layer properties, radiative and convective heat transfer about two hypersonic blunt bodies at zero angle of attack in assumed Martian atmosphere
Atmospheric gas composition effects on shock layer radiative heat transfer and heat shield response in Venus entry simulated by earth reentry
Mass injection effects on viscous hypersonic low Reynolds number shock layer downstream and at stagnation point in blunt forebody region analyzed for nonreacting gas
Viscous hypersonic shock layer over blunt bodies at low Reynolds number
Electron concentration profiles in blunt nose vehicle shock layer during atmospheric near orbital entry at high altitudes, using finite rate chemistry
Nonequilibrium ionized hypersonic flow over blunt body at low Reynolds number, using thin shock layer assumption in analysis
Nongray equilibrium radiative heat transfer in viscous radiating shock layer around blunt body entering high temperature nonisothermal carbon dioxide-nitrogen atmosphere
Rotational temperature and density measurements in rarefied flow over sharp leading edge flat plate, obtaining shock layer static pressure