Application of forebody strakes for directional stability and control of transport aircraft

23rd Atmospheric Flight Mechanics Conference

Volumn , Issue , 1998, Pages 650-658

  Shah, Gautam H ^a   Grandaf, J Nijel ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b BOEING COMPANY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT CONTROL; ANGLE OF ATTACK; NASA; TRANSPORT AIRCRAFT; WIND TUNNELS;

AIRCRAFT CONFIGURATIONS; ANGLES OF ATTACK; DIRECTIONAL STABILITY; LOW-SPEED WIND TUNNEL; PARAMETRIC VARIATION; RESEARCH EFFORTS; TECHNOLOGY RESEARCH; YAW CONTROL;

FLIGHT CONTROL SYSTEMS;

EID: 84983161173     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (3)

1. Murri, D. G.; Fisher, D. F.; and Lanser, W. R.: Flight-Test Results of Actuated Forebody Strake Controls on the F-18 High-Alpha Research Vehicle. NASA CP-1998-207676, Part 2, June, 1998.
2. Fisher, D. F.; Murri, D. G.; and Lanser, W. R.: Effect of Actuated Forebody Strakes on the Forebody Aerodynamics of the NASA F-18 HARV. NASA CP-1998-207676, Part 2, June, 1998.
3. Lin, J. C.; Robinson, S. K.; McGhee, R. J.; and Valarezo, W. O.: Separation Control on High Reynolds Number Multi-Element Airfoils. AIAA-92-2636, June, 1992.