Author: Bernard G. Gautier
Publisher:
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. Gautier
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100
Book Description
Publisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 100
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 882
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.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 882
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.
Shock Wave - Turbulent Boundary Layer Interaction in High Speed Flow
Author: Michael S. Holden
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 188
Book Description
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 188
Book Description
The Aeronautical Journal
Laminar and Turbulent Separation Including Three-dimensional Effects
Author: Von Karman Institute for Fluid Dynamics
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 254
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 254
Book Description
Improved Computer Program for Calculation of Viscous-inviscid Interactions
Author: Bernard G. Gautier
Publisher:
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).
Publisher:
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).
A Collection of Technical Papers
Government Reports Announcements
Government Reports Announcements & Index
Report of the Research and Other Activities
Author: California Institute of Technology. Division of Engineering and Applied Science
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 726
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 726
Book Description