Author: Marcus O. CreagerPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36
Book Description
Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7
Author: Marcus O. CreagerPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 36
Book Description
Effect of Leading-edge Thickness on the Flow Over a Flat Plate at a Mach Number of 5.7
Author: Marcus O. CreagerPublisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
The Leading Edge Effect on the Flow Over a Flat Plate at M
Author: James Courtland TownsendPublisher:
ISBN:
Category :
Languages : en
Pages : 70
Book Description
A study of the leading edge effects on the flow over a flat plate was made at a Mach number of 10. The Reynolds number based on free stream conditions and leading edge thickness varied from 115, where viscous effects predominated, to 14,550, where inviscid effects predominated. Shock wave shape and pressure and heat transfer distributions over the plate were obtained. In general, good agreement existed between the measurements and the various theories. The use of appropriate parameters allowed the results to be compared with those of a similar study using helium as the test fluid. Good correlation was found between the measurements made in air and in helium. (Author).
The Leading-edge Effects on the Laminar Flat-plate Boundary Layer and the Aerodynamic Heating at Mach 10.4
Author: Howard W. StonePublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44
Book Description
NASA Technical Note
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 534
Book Description
The Flow Field Over Blunted Flat Plates and Its Effect on Turbulent Boundary-layer Growth and Heat Transfer at a Mach Number of 4.7
Author: Thorval TendelandPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 64
Book Description
WADC Technical Report
Author: United States. Wright Air Development DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1502
Book Description
Some Simple Solutions to the Problem of Predicting Boundary-layer Self-induced Pressures
Author: Michael H. BertramPublisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 58
Book Description
Effects of Mach Number, Leading Edge Bluntness and Sweep on Boundary-layer Transition on a Flat Plate
Author: Don W. JilliePublisher:
ISBN:
Category : Fluid mechanics
Languages : en
Pages : 36
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
