Flight stability and control tests of scale model of four-duct tandem V/STOL aircraf
The NASA Langley transonic dynamics tunnel, which has a variable density Freon-12 (or air) test medi...
Comparative evaluation of interference factor corrections in wind tunnel tests on vertical takeoff a...
"The investigation consisted of free-flight model tests in hovering and forward flight through the t...
Dynamic stability and control characteristics of 0.18 scale model of fan-in-wing VTOL aircraf
An experimental investigation was made of the static and dynamic stability characteristics of a one-...
Wind tunnel stability and control tests of flexible wing manned aircraft - parawin
Force tests to determine static and dynamic longitudinal stability derivatives of powered scale mode...
An overview of dynamic test techniques used at NASA Langley Research Center on scale models to obtai...
The Langley Impact Dynamics Research Facility (IDRF) was modified to obtain static force and moment ...
An investigation of the stability and control of a low-wing four-engine transport vertical-take-off ...
An investigation of the stability and control of a high-wing transport vertical-take-off airplane wi...
V/tol aircraft flight test with unshrouded propellers - static & dynamic stability during hovering &...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
Static and dynamic longitudinal stability tests of fan in wing V/STOL aircraft mode
Flight stability and control tests of scale model of four-duct tandem V/STOL aircraf
The NASA Langley transonic dynamics tunnel, which has a variable density Freon-12 (or air) test medi...
Comparative evaluation of interference factor corrections in wind tunnel tests on vertical takeoff a...
"The investigation consisted of free-flight model tests in hovering and forward flight through the t...
Dynamic stability and control characteristics of 0.18 scale model of fan-in-wing VTOL aircraf
An experimental investigation was made of the static and dynamic stability characteristics of a one-...
Wind tunnel stability and control tests of flexible wing manned aircraft - parawin
Force tests to determine static and dynamic longitudinal stability derivatives of powered scale mode...
An overview of dynamic test techniques used at NASA Langley Research Center on scale models to obtai...
The Langley Impact Dynamics Research Facility (IDRF) was modified to obtain static force and moment ...
An investigation of the stability and control of a low-wing four-engine transport vertical-take-off ...
An investigation of the stability and control of a high-wing transport vertical-take-off airplane wi...
V/tol aircraft flight test with unshrouded propellers - static & dynamic stability during hovering &...
The optimal control model for pilot vehicle systems was used to develop a methodology for predicting...
Static and dynamic longitudinal stability tests of fan in wing V/STOL aircraft mode
Flight stability and control tests of scale model of four-duct tandem V/STOL aircraf
The NASA Langley transonic dynamics tunnel, which has a variable density Freon-12 (or air) test medi...
Comparative evaluation of interference factor corrections in wind tunnel tests on vertical takeoff a...