Add to ORKGAerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from Mach 0.4 to 1.
Wind tunnel tests to determine subsonic stability and control effectiveness of straight and delta wi...
A 0.015 scale model of a modified version of the MDAC space shuttle booster was tested in the Naval ...
An investigation was conducted in the Langley low-turbulence pressure tunnel to determine Reynolds n...
Wind tunnel tests of delta wing space shuttle orbiter to obtain force and stability data at high ang...
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle model
This test program was the first wind tunnel investigation of a double delta wing space shuttle orbit...
Longitudinal, lateral, and directional static stability and control characteristics of delta wing sp...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
Wind tunnel tests of delta wind and straight wing space shuttle orbiter models to determine static s...
Two 0.00325-scale models of a space shuttle orbiter were tested in trisonic wind tunnel to obtain fo...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
Wind tunnel tests to determine subsonic stability and control effectiveness of straight and delta wi...
A 0.015 scale model of a modified version of the MDAC space shuttle booster was tested in the Naval ...
An investigation was conducted in the Langley low-turbulence pressure tunnel to determine Reynolds n...
Wind tunnel tests of delta wing space shuttle orbiter to obtain force and stability data at high ang...
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle model
This test program was the first wind tunnel investigation of a double delta wing space shuttle orbit...
Longitudinal, lateral, and directional static stability and control characteristics of delta wing sp...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
Wind tunnel tests of delta wind and straight wing space shuttle orbiter models to determine static s...
Two 0.00325-scale models of a space shuttle orbiter were tested in trisonic wind tunnel to obtain fo...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
Wind tunnel tests to determine subsonic stability and control effectiveness of straight and delta wi...
A 0.015 scale model of a modified version of the MDAC space shuttle booster was tested in the Naval ...
An investigation was conducted in the Langley low-turbulence pressure tunnel to determine Reynolds n...