Add to ORKGProcedures and methods for predicting aerothermodynamic heating to delta orbiter shuttle vehicles we...
Subsonic longitudinal andd laternal directional characteristics were obtained for several modified c...
The collection and analysis of aerodynamic heating data obtained from shock impingement experimental...
Predicted and measured aerodynamic characteristics for blended delta-wing orbiter at hypersonic spee...
The heating on a candidate hypersonic research airplane configuration has been examined experimental...
Design of an efficient thermal protection system for the space shuttle orbiter and booster is discus...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
This test program was the first wind tunnel investigation of a double delta wing space shuttle orbit...
The unsteady aerodynamics of the proposed delta planform, high cross range, shuttle orbiters, are in...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
The phase change paint technique was used to make heat transfer measurements on the windward wing/el...
The lee-surface flow phenomena on a delta-wing orbiter and a straight-wing orbiter have been investi...
An investigation was conducted in the Langley low-turbulence pressure tunnel to determine Reynolds n...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
Entry heating flight data and wind tunnel data on the lower windward and upper lee side centerline, ...
Procedures and methods for predicting aerothermodynamic heating to delta orbiter shuttle vehicles we...
Subsonic longitudinal andd laternal directional characteristics were obtained for several modified c...
The collection and analysis of aerodynamic heating data obtained from shock impingement experimental...
Predicted and measured aerodynamic characteristics for blended delta-wing orbiter at hypersonic spee...
The heating on a candidate hypersonic research airplane configuration has been examined experimental...
Design of an efficient thermal protection system for the space shuttle orbiter and booster is discus...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
This test program was the first wind tunnel investigation of a double delta wing space shuttle orbit...
The unsteady aerodynamics of the proposed delta planform, high cross range, shuttle orbiters, are in...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
The phase change paint technique was used to make heat transfer measurements on the windward wing/el...
The lee-surface flow phenomena on a delta-wing orbiter and a straight-wing orbiter have been investi...
An investigation was conducted in the Langley low-turbulence pressure tunnel to determine Reynolds n...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
Entry heating flight data and wind tunnel data on the lower windward and upper lee side centerline, ...
Procedures and methods for predicting aerothermodynamic heating to delta orbiter shuttle vehicles we...
Subsonic longitudinal andd laternal directional characteristics were obtained for several modified c...
The collection and analysis of aerodynamic heating data obtained from shock impingement experimental...