Author: K. S. HeffnerPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Leading Edge Effect on Rarefied Hypersonic Flow Over a Flat Plate
Author: K. S. HeffnerPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Studies of the Leading Edge Effect on the Rarefied Hypersonic Flow Over a Flat Plate
Author: William Whyte JossPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 7
Book Description
Local Leading Edge Heat Transfer on a Flat Plate in Rarefied Hypersonic Flow
Author: James David HendryPublisher:
ISBN:
Category :
Languages : en
Pages : 80
Book Description
The local heat flux to a sharp edged flat plate was measured over the range 32.8
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
Heat Transfer on a Flat Plate in Continuum to Rarefied Hypersonic Flows at Mach Numbers of 19.2 and 25.4
Author: Henry T. NagamatsuPublisher:
ISBN:
Category : Heat
Languages : en
Pages : 68
Book Description
Interference Effects on the Hypersonic, Rarefied Flow about a Flat Plate
Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 42
Book Description
An Experimental Study of the Effects of Small Leading Edge Thickness on the Development of the Hypersonic Rarefied Flow Over a Flat Plate
Author: William Whyte JossPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages :
Book Description
Interference Effects on the Hypersonic, Rarefied Flow about a Flat Plate
Author: National Aeronautics and Space Administration (NASA)Publisher: Createspace Independent Publishing Platform
ISBN: 9781722316297
Category :
Languages : en
Pages : 38
Book Description
The Direct Simulation Monte Carlo method is used to study the hypersonic, rarified flow interference effects on a flat plate caused by nearby surfaces. Calculations focus on shock-boundary-layer and shock-lip interactions in hypersonic inlets. Results are presented for geometries consisting of a flat plate with different leading-edge shapes over a flat lower wall and a blunt-edge flat plate over a 5-degree wedge. The problems simulated correspond to a typical entry flight condition of 7.5 km/s at altitudes of 75 to 90 km. The results show increases in predicted local heating rates for shock-boundary-layer and shock-lip interactions that are quantitatively similar to those observed experimentally at much higher densities. Wilmoth, Richard G. Langley Research Center RTOP 506-40-91-02...
Effect of Slight Blunting of Leading Edge of an Immersed Body on the Flow Around it at Hypersonic Speeds
Author: Goromir Goromirovich ChernyĭPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 24
Book Description
Effect of Slip on the Laminar Boundary Layer Near the Leading Edge of a Flat Plate in Hypersonic Rarefied Gas Flow
Author: ROBERT E. STREETPublisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
