Flight measurements of downwash on the Ball-Bartoe Jetwing powered lift aircraft

Author:

Solies U. P.1

Affiliation:

1. University of Tennessee Space Institute, Tullahoma, Tennessee 37388

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference20 articles.

1. Items 4-7 were displayed on standard instruments; the other data were also readily available from special instrumentation that had been installed in the aircraft for previously conducted flight test programs. A detailed description of the instrumentation set up in the test vehicle can be found in Ref. 12.

2. The Lift on a Thin Aerofoil with a Jet-Augmented Flap

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2. Numerical Assessment of Pneumatic Devices on the Wing/Fuselage Junction of a Tiltrotor;Journal of Aircraft;2013-05

3. Multidisciplinary design optimization of blended-wing-body transport aircraft with distributed propulsion;Aerospace Science and Technology;2013-03

4. MDO of a Blended-Wing-Body Transport Aircraft with Distributed Propulsion;AIAA's 3rd Annual Aviation Technology, Integration, and Operations (ATIO) Forum;2003-06-21

5. Graduate education in flight testing;6th AIAA Biennial Flight Test Conference;1992-08-17

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