Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 704
Book Description
Scientific and Technical Aerospace Reports
Author: NASA Technical Note
Author: Power-law Velocity-profile-exponent Variations with Reynolds Number, Wall Cooling, and Mach Number in a Turbulent Boundary Layer
Author: Charles Borden JohnsonPublisher:
ISBN:
Category : Reynolds number
Languages : en
Pages : 66
Book Description
U.S. Government Research Reports
Author: Dominance of Radiated Aerodynamic Noise on Boundary-layer Transition in Supersonic-hypersonic Wind Tunnels
Author: Samuel R. PatePublisher:
ISBN:
Category : Aerodynamic noise
Languages : en
Pages : 418
Book Description
An experimental investigation was conducted to determine the effects of radiated aerodynamic-noise on boundary-layer transition in supersonic-hypersonic wind tunnels. It is conclusively shown that the aerodynamic noise (pressure fluctuations associated with sound waves), which radiate from the tunnel wall, turbulent boundary layer, will dominate the transition process on sharp flat places and sharp slender cones at zero incidence.
Technical Abstract Bulletin
Author: NASA Technical Paper
Author: Index to NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
A Summary of Information on Support Interference at Transonic and Supersonic Speeds
Author: Eugene S. LovePublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description
Abstract: A compilation of available information on the problem of support interference at transonic and supersonic speeds is presented.
Author: