Add to ORKGWind tunnel tests of delta wing space shuttle orbiter to obtain force and stability data at high angles of attack and blockage free condition
Low speed wind tunnel tests of subsonic aerodynamic properties of generic high cross range shuttle o...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle model
Wind tunnel tests of delta wind and straight wing space shuttle orbiter models to determine static s...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
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...
Two 0.00325-scale models of a space shuttle orbiter were tested in trisonic wind tunnel to obtain fo...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel...
The test was a conventional stability and control test except for two aspects. One was the very high...
Low speed wind tunnel tests of subsonic aerodynamic properties of generic high cross range shuttle o...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
Trisonic wind tunnel static stability tests on straight wing and delta wing space shuttle model
Wind tunnel tests of delta wind and straight wing space shuttle orbiter models to determine static s...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
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...
Two 0.00325-scale models of a space shuttle orbiter were tested in trisonic wind tunnel to obtain fo...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel...
The test was a conventional stability and control test except for two aspects. One was the very high...
Low speed wind tunnel tests of subsonic aerodynamic properties of generic high cross range shuttle o...
Low speed wind tunnel test to define space shuttle model cruise and landing aerodynamic characterist...
An investigation has been conducted in the Langley Unitary Plan wind tunnel to determine the static ...