Author: Fang-Jenq ChenPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 60
Book Description
Correlations of Supersonic Boundary-layer Transition on Cones Including Effects of Large Axial Variations in Wind-tunnel Noise
Author: Fang-Jenq ChenPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 60
Book Description
Correlations of Supersonic Boundary-layer Transition on Cones Including Effects of Large Axial Variations in Wind-tunnel Noise
Author: Fang-Jenq ChenPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 60
Book Description
NASA Technical Paper
Author: Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 398
Book Description
Scientific and Technical Aerospace Reports
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1390
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Boundary Layer Transition at Supersonic Speeds
Author: E. R. Van DriestPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 108
Book Description
Experiments carried out in the 12-inch supersonic wind tunnel to investigate the effect of three dimensional roughness elements (spheres) on boundary-layer transition on a 10-degree (apex angle) cone without heat transfer are described. The local Mach number for these tests was 2.71. The data show clearly that the minimum (effective) size of trip required to bring transition to its lowest Reynolds number varies power of the distance from the apex of the cone to the trip. Use of available data at other Mach numbers indicates that the Mach number influence for effective tripping is taken into account by a simple expression. Some remarks concerning the roughness variation for transition on a blunt body are made. Finally, a general criterion is introduced which gives insight to the transition phenomenon and anticipates effects of external and internal disturbances, Mach number transfer.
A Correlation of Artifically Induced Boundary-layer Transition Data from Blunt Slender Cones at Hypersonic Speeds
Author: Albert H. BoudreauPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 18
Book Description
NASA Scientific and Technical Publications
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 410
Book Description
New Results in Numerical and Experimental Fluid Mechanics III
Author: Siegfried WagnerPublisher: Springer Science & Business Media
ISBN: 3540454667
Category : Technology & Engineering
Languages : en
Pages : 431
Book Description
This volume contains the papers of a German symposium dealing with research and project work in numerical and experimental aerodynamics and fluidmechanics for aerospace and other applications. It gives a broad overview over the ongoing work in this field in Germany.
Monthly Catalogue, United States Public Documents
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1252
Book Description
Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 974
Book Description
