Author: Robert Allan WhitePublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 216
Book Description
Turbulent Boundary Layer Separation from Smooth-convex Surfaces in Supersonic Two-dimensional Flow
Author: Robert Allan WhitePublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 216
Book Description
Incipient Separation of a Turbulent Boundary Layer at High Reynolds Number in Two- Dimensional Supersonic Flow Over a Compression Corner
Author: The Effects of Convex Surface Curvature on Boundary Layer Separation in Supersonic Flow
Author: Turbulent Flow Separation Ahead of Forward Facing Steps in Supersonic Two Dimensional and Axisymmetric Flows
Author: Helmut T. UebelhackPublisher:
ISBN:
Category : Turbulence
Languages : en
Pages : 52
Book Description
Laminar and Turbulent Separation Including Three-dimensional Effects
Author: Von Karman Institute for Fluid DynamicsPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 254
Book Description
Advances in Heat Transfer
Author: Publisher: Academic Press
ISBN: 0080575609
Category : Science
Languages : en
Pages : 591
Book Description
Advances in Heat Transfer
Two-Dimensional Turbulent Boundary Layer Separation on a Flat Plate with Ramp at Freestream Mach Numbers of 3.7 and 6.3 in Supersonic and Hypersonic Flow
Author: Victor ZakkayPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description
This investigation describes surface pressure distribution, heat transfer, and turbulent flow separation and reattachment on a flat plate with variable ramp angle at Mach numbers averaging 3.66 and 6.30. The freestream Reynold's number varied from 3.33 to 8.34 million per foot for the former case and from 5.243 million to 14.6 million per foot for the latter case. Ramp angle was varied from 0 to 35 degrees for these experiments. Stagnation temperatures averaged 849 degrees Rankine, with wall temperature assumed constant at 535 degrees Rankine for all tests. The knowledge of effective wedge angles and freestream conditions makes it possible to determine shocks so that conditions can be evaluated at all positions on the model.
An Experimental Investigation of Turbulent Boundary Layers Along Curved Surfaces
Author: Ronald M. C. SoPublisher:
ISBN:
Category : Turbulent boundary layer
Languages : en
Pages : 276
Book Description
Boundary Layer Separation in Two-dimensional Supersonic Flow
Author: Aeronautical Research CouncilPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 8
Book Description
Author: