Add to ORKGProgress on experimental program using jet flapped wing model in wind tunnel facilities for testing V/STOL aircraf
Wind tunnel stability and control tests of flexible wing manned aircraft - parawin
Aerodynamic characteristics of V/STOL transport model with wing-mounted lift fans - large-scale wind...
Wind tunnel tests on a finite, knee-blowing-flapped wing and on a direct jet lift configuration were...
Feasibility of V/STOL test section in wind tunnel by using one eighth scale model of tunne
Comparative evaluation of interference factor corrections in wind tunnel tests on vertical takeoff a...
Large scale wind tunnel tests of airplane model with rotating cylinder flaps and four propeller
Tests were made in the Ames 40- by 80-foot wind tunnel to determine the forward speed effects on win...
A propulsive wing/canard model was tested at STOL operating conditions in the NASA Langley Research ...
The basic concepts of wind-tunnel boundary interference are discussed and the development of the the...
Wind tunnel wall effects and wall corrections for vertical short takeoff and landing tilt-wing model...
The NASA Langley Transonic Dynamics Tunnel, which has a variable density, Freon-12 (or air) test med...
The NASA Langley transonic dynamics tunnel, which has a variable density Freon-12 (or air) test medi...
A status report and review of wind tunnel model experimental techniques that have been developed to ...
The ability of current methodologies to accurately predict the aerodynamic characteristics identifie...
A STOL fighter model employing the vectored-engine-over wing concept was tested at low speeds in the...
Wind tunnel stability and control tests of flexible wing manned aircraft - parawin
Aerodynamic characteristics of V/STOL transport model with wing-mounted lift fans - large-scale wind...
Wind tunnel tests on a finite, knee-blowing-flapped wing and on a direct jet lift configuration were...
Feasibility of V/STOL test section in wind tunnel by using one eighth scale model of tunne
Comparative evaluation of interference factor corrections in wind tunnel tests on vertical takeoff a...
Large scale wind tunnel tests of airplane model with rotating cylinder flaps and four propeller
Tests were made in the Ames 40- by 80-foot wind tunnel to determine the forward speed effects on win...
A propulsive wing/canard model was tested at STOL operating conditions in the NASA Langley Research ...
The basic concepts of wind-tunnel boundary interference are discussed and the development of the the...
Wind tunnel wall effects and wall corrections for vertical short takeoff and landing tilt-wing model...
The NASA Langley Transonic Dynamics Tunnel, which has a variable density, Freon-12 (or air) test med...
The NASA Langley transonic dynamics tunnel, which has a variable density Freon-12 (or air) test medi...
A status report and review of wind tunnel model experimental techniques that have been developed to ...
The ability of current methodologies to accurately predict the aerodynamic characteristics identifie...
A STOL fighter model employing the vectored-engine-over wing concept was tested at low speeds in the...
Wind tunnel stability and control tests of flexible wing manned aircraft - parawin
Aerodynamic characteristics of V/STOL transport model with wing-mounted lift fans - large-scale wind...
Wind tunnel tests on a finite, knee-blowing-flapped wing and on a direct jet lift configuration were...