Roll-yaw control at high angle of attack by forebody tangential blowing

An edition of Roll-yaw control at high angle of attack by forebody tangential blowing (1995)

Roll-yaw control at high angle of attack by forebody tangential blowing

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1995

Publisher

Joint Institute for Aeronautics and Acoustics,National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Blowing, Aircraft control, Feedback control, Roll, Flight control, Flow visualization, Wind tunnel models, Yawing moments, Wind tunnel tests