Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

Status

Rate

Check Later

Authors

William G. Johnson

William G. Johnson

Subjects

Boeing Aircraft Testing High Reynolds Number Supercritical Airfoils Aerodynamics Wind Tunnel Tests Transonic Aerodynamics Statistics Airfoil Profiles Cryogenic Wind Tunnels

Reviews (0) see more

Seems like you haven't provided a review

Don't miss the opportunity to share your thoughts!

Similar Books

Similar Movies

Similar TV Series

Similar Games