Zobrazeno 1 - 5
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pro vyhledávání: '"Wendy R. Lanser"'
Autor:
Larry A. Meyn, Wendy R. Lanser
Publikováno v:
Journal of Aircraft. 31:1365-1371
A full-scale F/A-18 was tested in the 80- by 120-Foot Wind Tunnel at NASA Ames Research Center to measure the effectiveness of pneumatic forebody vortex control devices. By altering the forebody vortex flow, yaw control can be maintained to angles of
Publikováno v:
10th Applied Aerodynamics Conference.
This paper presents an overview of high angle-of-attack tests of a full-scale F/A-18 in the 80- by 120-Foot Wind Tunnel of the National Full-Scale Aerodynamic Complex at NASA Ames Research Center at Moffett Field, California. A production aircraft wa
Publikováno v:
10th Applied Aerodynamics Conference.
A full aircraft geometry is used to computationally analyze the effectiveness of a pneumatic forebody flow control concept. An overset grid technique is employed to model the aircraft and slot geometry. Steady-state solutions for both isolated forebo
Publikováno v:
SAE Technical Paper Series.
The effectiveness of an aerodynamic boattail on a tractor/trailer road vehicle was measured in the NASA Ames Research Center 80- by 120-Foot Wind Tunnel. Results are examined for the tractor/trailer with and without the drag reduction device. Pressur
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