Microblowing for high-angle-of-attack vortex flow control on a fighter aircraft

Journal of Aircraft

Volumn 38, Issue 3, 2001, Pages 454-457

  Roos, F W ^a  

^a BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; FLOW CONTROL; OPTIMIZATION; VORTEX FLOW; WIND TUNNELS;

ANGLE OF ATTACK; MICROBLOWING; VORTEX FLOW CONTROL;

FIGHTER AIRCRAFT;

EID: 0035334098     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.2813     Document Type: Article

References (12)

1. A study of the effects of viscosity on flow over slender inclined bodies of revolution
2. Modern fighter aircraft design for high-angle-of-attack maneuvering
3. Forebody vortex control-a progress review
4. A review of forebody vortex control scenarios
5. Control of the forebody vortex orientation by asymmetric air injection
6. Bluntness and blowing for flowfield asymmetry control on slender forebodies
7. Investigation of side forces on Ogive-cylinder bodies at high angles of attack in the M = 0.5 to 1.1 range
8. A systematic study of the correlation between geometrical disturbances and flow asymmetries
9. Low-energy pneumatic control of forebody vortices
10. F-15 forebody vortex flow control using jet nozzle blowing
11. Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack
12. Effects of surface perturbations on the asymmetric vortex flow over a slender body