The X-29A aircraft is the first manned, experimental high-performance aircraft to be fabricated and flown in many years. The approach for expanding the X-29 flight envelope and collecting research data is described including the methods for monitoring wind divergence, flutter, and aeroservoelastic coupling of the aerodynamic forces with the structure and the flight-control system. Examples of the type of flight data to be acquired are presented along with types of aircraft maneuvers that will be flown. A brief description of the program management structure is also presented and the program schedule is discussed
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
A limited flight experiment was conducted to document the ground-effect characteristics of the X-29A...
Aerodynamic data from NASA Ames Research Center's 11-Foot Transonic Wind Tunnel are plotted for the ...
The X-29A aircraft is a fascinating combination of integrated technologies incorporated into a uniqu...
The X-29A research and technology demonstrator aircraft has completed a highly successful multiphase...
The X-29A advanced technology demonstrator flight envelope expansion program and the subsequent flig...
The X-29A advanced technology demonstrator is a single-seat, single-engine aircraft with a forward-s...
Flight research and testing form a critical link in the aeronautic R and D chain. Brilliant concepts...
Several new technologies integrated on the X-29A advanced technology demonstrator are being evaluate...
The X-29A subsonic lift and drag characteristics determined, met, or exceeded predictions, particula...
An overview of the X-29A functional flight program and concept evaluation program is presented, incl...
A brief description of the flight control system of the X-29A forward-swept-wing flight demonstrator...
The results of an integrated study of structures, aerodynamics, and controls using the STARS program...
This report contains numerous color illustrations to describe the NASA programs in aeronautics. The ...
From 1967 to 1997, pioneering propulsion flight research activities have been conceived and conducte...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
A limited flight experiment was conducted to document the ground-effect characteristics of the X-29A...
Aerodynamic data from NASA Ames Research Center's 11-Foot Transonic Wind Tunnel are plotted for the ...
The X-29A aircraft is a fascinating combination of integrated technologies incorporated into a uniqu...
The X-29A research and technology demonstrator aircraft has completed a highly successful multiphase...
The X-29A advanced technology demonstrator flight envelope expansion program and the subsequent flig...
The X-29A advanced technology demonstrator is a single-seat, single-engine aircraft with a forward-s...
Flight research and testing form a critical link in the aeronautic R and D chain. Brilliant concepts...
Several new technologies integrated on the X-29A advanced technology demonstrator are being evaluate...
The X-29A subsonic lift and drag characteristics determined, met, or exceeded predictions, particula...
An overview of the X-29A functional flight program and concept evaluation program is presented, incl...
A brief description of the flight control system of the X-29A forward-swept-wing flight demonstrator...
The results of an integrated study of structures, aerodynamics, and controls using the STARS program...
This report contains numerous color illustrations to describe the NASA programs in aeronautics. The ...
From 1967 to 1997, pioneering propulsion flight research activities have been conceived and conducte...
New flight test techniques in use at Ames Dryden are reviewed. The use of the pilot in combination w...
A limited flight experiment was conducted to document the ground-effect characteristics of the X-29A...
Aerodynamic data from NASA Ames Research Center's 11-Foot Transonic Wind Tunnel are plotted for the ...