The heat flux and boundary layers over a flat plate at suborbital and superorbital speeds were measured in a freepiston expansion tube at enthalpies of 26.0 and 53.4 MJ/kg, respectively. Estimates of the gas-phase and surface Damkohler numbers were made that indicate that although the boundary layer might be frozen, there is a possibility of surface reactions occurring. The heat-flux results were compared with theoretical predictions of heat flux for both frozen and equilibrium chemistries. The results indicated that the influence of real gas effects, such as recombination and surface catalycity, were minimal for the present flow conditions. Interferograms were obtained using resonance enhancement of the thermal boundary layer over a flat p...
We study the stagnation point boundary layer of high enthalpy subsonic flows obtained in inductively...
Boundary layer on a uniformly heated flat plate was studied experimentally. Both, the velocity bound...
Heat transfer and pressure on a flat plate and on protuberances in a supersonic turbulent boundary l...
Heat-transfer rates from a non-equilibrium hypersonic air flow to flat plates at zero and 12° incide...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
Heat transfer levels have been investigated behind a rearward-facing step in a superorbital expansio...
The boundary layer on a 5 deg. half-angle cone is studied by measurement of the heat flux distributi...
An experimental study of boundary layer on a flat plate with heat transfer was done. Temperature and...
The effect on transition of a non-adiabatic surface was systematically studied in the present experi...
Reactant concentrations in the diffusion-controlled flow over a surface of constant catalycity are c...
A Mach-10 hypersonic boundary layer of air overriding a cold, isothermal, non-catalytic flat wall, a...
Two dimensional fourth order boundary layer calculations were made for flows over a flat plate with ...
The successful operation of an acceleration-compensated skin-friction transducer in test times and a...
In a reacting gas flow both gas-phase chemical activity and surface catalysis can increase the rate ...
Heat transfer levels have been investigated behind a rearward-facing step in the X2 super-orbital ex...
We study the stagnation point boundary layer of high enthalpy subsonic flows obtained in inductively...
Boundary layer on a uniformly heated flat plate was studied experimentally. Both, the velocity bound...
Heat transfer and pressure on a flat plate and on protuberances in a supersonic turbulent boundary l...
Heat-transfer rates from a non-equilibrium hypersonic air flow to flat plates at zero and 12° incide...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
Heat transfer levels have been investigated behind a rearward-facing step in a superorbital expansio...
The boundary layer on a 5 deg. half-angle cone is studied by measurement of the heat flux distributi...
An experimental study of boundary layer on a flat plate with heat transfer was done. Temperature and...
The effect on transition of a non-adiabatic surface was systematically studied in the present experi...
Reactant concentrations in the diffusion-controlled flow over a surface of constant catalycity are c...
A Mach-10 hypersonic boundary layer of air overriding a cold, isothermal, non-catalytic flat wall, a...
Two dimensional fourth order boundary layer calculations were made for flows over a flat plate with ...
The successful operation of an acceleration-compensated skin-friction transducer in test times and a...
In a reacting gas flow both gas-phase chemical activity and surface catalysis can increase the rate ...
Heat transfer levels have been investigated behind a rearward-facing step in the X2 super-orbital ex...
We study the stagnation point boundary layer of high enthalpy subsonic flows obtained in inductively...
Boundary layer on a uniformly heated flat plate was studied experimentally. Both, the velocity bound...
Heat transfer and pressure on a flat plate and on protuberances in a supersonic turbulent boundary l...