Add to ORKGPressure data are presented in tabular form on the SRM booster of the space shuttle launch vehicle configuration model. For Vol. 3, see N75-23657
Data were obtained for Mach numbers from 0.6 to 3.48, angles of attack from -10 to 10 degrees, and a...
Wind tunnel tests of a 0.0405 scale model of the -1404A/B configuration of the Space Shuttle Vehicle...
Data obtained from the wind tunnel tests of a scale model of the space shuttle orbiter configuration...
Pressure data are presented in tabular form on the external tank base and SRM booster base of the sp...
Pressure data are presented in tabular form on the external tank and the SRM nozzle of the space shu...
Pressure data are presented in tabular form on the lower wing surface of the space shuttle launch ve...
Pressure data are presented in tabular form on the external tank attach points and the external tank...
Pressure data are presented in tabular form on the left and right vertical tail surface of the space...
Results of tests conducted on an 0.030-scale launch configuration model of the space shuttle vehicle...
The results of the tests are presented along with aerodynamic loads data obtained at Mach numbers fr...
Pressure data are presented in tabular form on the upper wing surface of the space shuttle launch ve...
The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...
A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...
Plots and tabular listings are presented for both force and pressure data for the upper wing
The results of wind tunnel tests of the 140A/B configuration components are reported for the fuselag...
Data were obtained for Mach numbers from 0.6 to 3.48, angles of attack from -10 to 10 degrees, and a...
Wind tunnel tests of a 0.0405 scale model of the -1404A/B configuration of the Space Shuttle Vehicle...
Data obtained from the wind tunnel tests of a scale model of the space shuttle orbiter configuration...
Pressure data are presented in tabular form on the external tank base and SRM booster base of the sp...
Pressure data are presented in tabular form on the external tank and the SRM nozzle of the space shu...
Pressure data are presented in tabular form on the lower wing surface of the space shuttle launch ve...
Pressure data are presented in tabular form on the external tank attach points and the external tank...
Pressure data are presented in tabular form on the left and right vertical tail surface of the space...
Results of tests conducted on an 0.030-scale launch configuration model of the space shuttle vehicle...
The results of the tests are presented along with aerodynamic loads data obtained at Mach numbers fr...
Pressure data are presented in tabular form on the upper wing surface of the space shuttle launch ve...
The investigations of pressure distributions are presented for aeroloads analysis at Mach numbers fr...
A wind tunnel test of an 0.030-scale space shuttle vehicle orbiter configuration 140A/B model was co...
Plots and tabular listings are presented for both force and pressure data for the upper wing
The results of wind tunnel tests of the 140A/B configuration components are reported for the fuselag...
Data were obtained for Mach numbers from 0.6 to 3.48, angles of attack from -10 to 10 degrees, and a...
Wind tunnel tests of a 0.0405 scale model of the -1404A/B configuration of the Space Shuttle Vehicle...
Data obtained from the wind tunnel tests of a scale model of the space shuttle orbiter configuration...