Sign In
Sign Up
-
/
5
0 votes
Share
Body and canard effects on an attached-flow maneuver wing at Mach 1.62
Status
Rate
Check Later
Authors
Jimmy L Pittman
Subjects
Aerodynamics
Wings
Canard
Supersonic
Supersonic Aerodynamics
Airplanes
Canard Wings
Reviews (0)
see more
Seems like you haven't provided a review
Don't miss the opportunity to
share your thoughts
!
Similar Books
see more
Similar Movies
see more
Similar TV Series
see more
Similar Games
see more