Add to ORKGStatic tests of augmentor-wing flap system for modified C-8A jet STOL research airplane using 0.7 scale mode
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
A 0.035-scale model fo a modified NKC-135 airplane was tested in 12-foot pressure wind tunnel to det...
Experimental investigations were performed in a 6- by 6-Foot Supersonic wind tunnel on a 0.015-scale...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
An experimental investigation was conducted in the Ames 14-foot transonic wind tunnel to study the a...
In-flight dynamic simulator used to evaluate problems of low-speed approach and landing of supersoni...
Investigation of space shuttle orbiter configurations 2A(VL70-000089B) and 3(VL70-000139B) was perfo...
The effect of various vertical tail arrangements upon the stability and control characteristics of a...
A project to develop an experimental aircraft for use as an inflight demonstrator of the augmentor w...
This report presents test procedures, methods, and instruments for flight testing of aircraft. Dynam...
Flight tests were conducted on the OS2U-2 seaplane with simple circular-arc-type ailerons directly c...
Biplane cellules using the N.A.C.A.-M6 airfoil section have been tested in the variable density wind...
An experimental investigation was conducted in an 11- by 11-foot transonic wind tunnel to study the ...
This report describes tests made for the purpose of determining the distribution of pressure over a ...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
A 0.035-scale model fo a modified NKC-135 airplane was tested in 12-foot pressure wind tunnel to det...
Experimental investigations were performed in a 6- by 6-Foot Supersonic wind tunnel on a 0.015-scale...
Report presents the results of an investigation of the general aerodynamic characteristics of the NA...
An experimental investigation was conducted in the Ames 14-foot transonic wind tunnel to study the a...
In-flight dynamic simulator used to evaluate problems of low-speed approach and landing of supersoni...
Investigation of space shuttle orbiter configurations 2A(VL70-000089B) and 3(VL70-000139B) was perfo...
The effect of various vertical tail arrangements upon the stability and control characteristics of a...
A project to develop an experimental aircraft for use as an inflight demonstrator of the augmentor w...
This report presents test procedures, methods, and instruments for flight testing of aircraft. Dynam...
Flight tests were conducted on the OS2U-2 seaplane with simple circular-arc-type ailerons directly c...
Biplane cellules using the N.A.C.A.-M6 airfoil section have been tested in the variable density wind...
An experimental investigation was conducted in an 11- by 11-foot transonic wind tunnel to study the ...
This report describes tests made for the purpose of determining the distribution of pressure over a ...
Report presents the results of tests conducted on 28 wing-fuselage combinations made in the variable...
At the request of the Army Air Corps, an investigation of the pressure distribution over PW-9 wing m...
A 0.035-scale model fo a modified NKC-135 airplane was tested in 12-foot pressure wind tunnel to det...
Experimental investigations were performed in a 6- by 6-Foot Supersonic wind tunnel on a 0.015-scale...