Author: Roberto Vaglio-LaurinPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 54
Book Description
Turbulent Heat Transfer on Blunt-nosed Bodies in Two-dimensional and General Three-dimensional Hypersonic Flow
Author: Roberto Vaglio-LaurinPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 54
Book Description
Turbulent Heat Transfer on Blunt-nosed Bodies in Two-dimensional and General Three-dimensional Hypersonic Flow
Author: Roberto Vaglio-LaurinAnalysis of the Three-dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow
Author: John C. AdamsPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 98
Book Description
An analytical approach toward numerical calculation of the three-dimensional turbulent boundary layer on a sharp cone at incidence under supersonic and hypersonic flow conditions is presented. The theoretical model is based on implicit finite-difference integration of the governing three-dimensional turbulent boundary-layer equations in conjunction with a three-dimensional scalar eddy-viscosity model of turbulence. Comparison is made of present theory with detailed experimental measurements of the three-dimensional turbulent boundary-layer structure (velocity and temperature profiles), the surface streamline direction (obtained via an oil-flow technique) and surface heat-transfer rate.
Engineering Design Handbook
Author: United States. Army Materiel CommandPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 108
Book Description
NASA Technical Note
Author: An Investigation of Laminar, Transitional and Turbulent Heat Transfer on Blunt-nosed Bodies in Hypersonic Flow
Author: Robert J. CresciPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 60
Book Description
Hypersonic Lifting Body Windward Surface Flow-field Analysis for High Angles of Incidence
Author: John C. Adams (Jr.)Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 240
Book Description
Formulation and application of a windward surface flow-field (inviscid and viscous) analysis is presented for general lifting body configurations at high angles of incidence under hypersonic perfect gas conditions. The technique applies a strip theory concept, leading to an infinite extent yawed body treatment applied in the windward surface crossflow plane for both the inviscid and viscous (boundary layer) flow fields. The boundary-layer analysis is based on the governing equations for yawed blunt body boundary layers.
Laminar, Transitional, and Turbulent Heat Transfer to a Cone-cylinder-flare Body at Mach 8.0
Author: Victor ZakkayPublisher:
ISBN:
Category : Boundary layer
Languages : en
Pages : 86
Book Description
A modified equation for the heat transfer coefficient in the transitional and fully turbulent region based on the F.P.R.E. method is then presented. This method gives good agreement with the experimental results presented here.
AIAA 74-550 - AIAA 74-603 (With omissions in numbering)
Author: Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1540
Book Description