Author: Bernard G. GautierPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100
Book Description
A Theoretical Study of Wall Cooling Effects Upon Shock Wave-laminar Boundary Layer Interaction by the Method of Lees-reeves-klineberg
Author: Bernard G. GautierPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100
Book Description
Scientific and Technical Aerospace Reports
Author: A Theoretical Study of Wall Cooling Effects Upon Shock Wave-laminar Boundary Layer Interaction
Author: Bernard G. GautierPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages :
Book Description
Shock Wave - Turbulent Boundary Layer Interaction in High Speed Flow
Author: Michael S. HoldenPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 188
Book Description
The Aeronautical Journal
Author: Laminar and Turbulent Separation Including Three-dimensional Effects
Author: Von Karman Institute for Fluid DynamicsPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 254
Book Description
A Parametric Study of Adiabatic Laminar Boundary Layer - Shock Wave Interactions by the Methods of Lees - Reeves - Klineberg
Author: M. L. RiethmullerImproved Computer Program for Calculation of Viscous-inviscid Interactions
Author: Bernard G. GautierPublisher:
ISBN:
Category : Viscous flow
Languages : en
Pages : 250
Book Description
The report describes a theoretical and experimental investigation of the effect of wall cooling on the overall features of shock wave laminar boundary layer interactions in hypersonic two dimensional flow. The integral method of Lees-Reeves-Klineberg has been modified in order to compute viscous interactions over a continuous range of wall-to-stagnation temperature ratios using a single set of 'universal' integral functions. Comparisons between the theoretical predictions and the experimental results obtained from pressure and heat transfer distribution measurements show satisfactory agreements. (Modified author abstract).
Author: 
Author: