Add to ORKGTrisonic wind tunnel static stability tests on straight wing and delta wing space shuttle model
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel...
Wind tunnel tests to determine aerodynamic effects of various spoilers and vortex generators install...
A wind tunnel test of an 0.030 scale model of the Rockwell International Configuration 140A/B Space ...
Wind tunnel tests of delta wind and straight wing space shuttle orbiter models to determine static s...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
Wind tunnel tests of delta wing space shuttle orbiter to obtain force and stability data at high ang...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
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...
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...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
Wind tunnel tests to determine subsonic stability and control effectiveness of straight and delta wi...
Low speed wind tunnel tests of effects of nacelle position, refaired fuelage, and elevator effective...
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel...
Wind tunnel tests to determine aerodynamic effects of various spoilers and vortex generators install...
A wind tunnel test of an 0.030 scale model of the Rockwell International Configuration 140A/B Space ...
Wind tunnel tests of delta wind and straight wing space shuttle orbiter models to determine static s...
Aerodynamic force and static stability data for scale model of space shuttle delta-wing orbiter from...
Wind tunnel tests of delta wing space shuttle orbiter to obtain force and stability data at high ang...
Experimental aerodynamic investigations have been made on a .0035 scale model North American Rockwel...
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...
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...
Low speed wind tunnel tests on longitudinal and lateral stability of high cross range delta wing spa...
An experimental aerodynamic wind tunnel investigation was conducted employing a 0.00325 scale model ...
Wind tunnel tests to determine subsonic stability and control effectiveness of straight and delta wi...
Low speed wind tunnel tests of effects of nacelle position, refaired fuelage, and elevator effective...
Experimental aerodynamic investigations were conducted at the MSFC 14 x 14 inch trisonic wind tunnel...
Wind tunnel tests to determine aerodynamic effects of various spoilers and vortex generators install...
A wind tunnel test of an 0.030 scale model of the Rockwell International Configuration 140A/B Space ...