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space shuttle orbiterMilitary unit
Analytical studies have been conducted concerning the lee-surface flow phenomena over a space shuttle orbiter model based on the experimental data obtained during September, 1971 through August, 1972. Lee-surface peak heating phenomena and flow separation patterns were analyzed. Major results of analyses are briefly presented
Aerothermodynamic tests of Phase B space shuttle configurations proposed by North American Rockwell/...
The collection and analysis of aerodynamic heating data obtained from shock impingement experimental...
Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Marti...
Surface pressure and heat transfer, flow separation, flow field, and oil flow patterns on the leewar...
The lee-surface flow phenomena on a delta-wing orbiter and a straight-wing orbiter have been investi...
Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamb...
The theoretical heat-transfer distributions are compared with experimental heat-transfer distributio...
The research for determining the space shuttle aerothermal environment is reported. Brief summaries ...
An experimental study has been conducted of the influence of wall to total temperature ratio on the ...
Discrepancies between experiment and computation for shuttle leeside flow separation, which came to ...
A broad base of thermocouple and phase change paint data was assembled and correlated to the nominal...
As a preliminary step toward predicting the leeside thermal environment for winged reentry vehicles ...
Procedures and methods for predicting aerothermodynamic heating to delta orbiter shuttle vehicles we...
The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the c...
Conference on aerodynamic heat transfer in space shuttle configurations and procedures and technique...
Aerothermodynamic tests of Phase B space shuttle configurations proposed by North American Rockwell/...
The collection and analysis of aerodynamic heating data obtained from shock impingement experimental...
Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Marti...
Surface pressure and heat transfer, flow separation, flow field, and oil flow patterns on the leewar...
The lee-surface flow phenomena on a delta-wing orbiter and a straight-wing orbiter have been investi...
Heating rate and pressure measurements were obtained on a 25-O space shuttle model in a vacuum chamb...
The theoretical heat-transfer distributions are compared with experimental heat-transfer distributio...
The research for determining the space shuttle aerothermal environment is reported. Brief summaries ...
An experimental study has been conducted of the influence of wall to total temperature ratio on the ...
Discrepancies between experiment and computation for shuttle leeside flow separation, which came to ...
A broad base of thermocouple and phase change paint data was assembled and correlated to the nominal...
As a preliminary step toward predicting the leeside thermal environment for winged reentry vehicles ...
Procedures and methods for predicting aerothermodynamic heating to delta orbiter shuttle vehicles we...
The aerothermodynamic performance of the Space Shuttle Orbiter during reentry is assessed from the c...
Conference on aerodynamic heat transfer in space shuttle configurations and procedures and technique...
Aerothermodynamic tests of Phase B space shuttle configurations proposed by North American Rockwell/...
The collection and analysis of aerodynamic heating data obtained from shock impingement experimental...
Aerothermodynamic tests of Phase B space shuttle configurations proposed by McDonnell Douglas--Marti...
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