Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6

Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6 PDF Author: Aubrey M. Cary
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 58

Get Book Here

Book Description

Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6

Turbulent-boundary-layer Heat-transfer and Transition Measurements with Surface Cooling at Mach 6 PDF Author: Aubrey M. Cary
Publisher:
ISBN:
Category : Heat
Languages : en
Pages : 58

Get Book Here

Book Description


A Review of High-speed, Convective, Heat-transfer Computation Methods

A Review of High-speed, Convective, Heat-transfer Computation Methods PDF Author: Michael E. Tauber
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 44

Get Book Here

Book Description


NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 960

Get Book Here

Book Description


Numerical Solution of the Equations for Compressible Laminar, Transitional, and Turbulent Boundary Layers and Comparisons with Experimental Data

Numerical Solution of the Equations for Compressible Laminar, Transitional, and Turbulent Boundary Layers and Comparisons with Experimental Data PDF Author: Julius E. Harris
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 92

Get Book Here

Book Description
A numerical method for solving the equations for laminar, transitional, and turbulent compressible boundary layers for either planar or axisymmetric flows is presented. The fully developed turbulent region is treated by replacing the Reynolds stress terms with an eddy viscosity model. The mean properties of the transitional boundary layer are calculated by multiplying the eddy viscosity by an intermittency function based on the statistical production and growth of the turbulent spots. A specifiable turbulent Prandtl number relates the turbulent flux of heat to the eddy viscosity. A three-point implicit finite-difference scheme is used to solve the system of equations. The momentum and energy equations are solved simultaneously without iteration. Numerous test cases are compared with experimental data for supersonic and hypersonic flows; these cases include flows with both favorable and mildly unfavorable pressure gradient histories, mass flux at the wall, and traverse curvature.

NASA Technical Report

NASA Technical Report PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 630

Get Book Here

Book Description


Survey of Boundary Layer Heat Transfer at High Velocities and High Temperatures

Survey of Boundary Layer Heat Transfer at High Velocities and High Temperatures PDF Author: Ernst Rudolf Georg Eckert
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 118

Get Book Here

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 130

Get Book Here

Book Description


WADC Technical Report

WADC Technical Report PDF Author: United States. Wright Air Development Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1276

Get Book Here

Book Description


Research Review

Research Review PDF Author:
Publisher:
ISBN:
Category : Research
Languages : en
Pages : 44

Get Book Here

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 840

Get Book Here

Book Description