Hypersonic and Other Viscous Interactions. Appendix A. Three-Dimensional Viscous Interactions.

Abstract

A study has been made of transpiration cooling of typical hypersonic re-entry configurations with a primary emphasis on experimental data acquisition, although some limited analytical and numerical support studies have been undertaken. The experiments have been conducted in the hypersonic flow region, under zero and non-zero angle of attack conditions, and covering the range in Reynolds numbers required to obtain laminar, transitional, and turbulent data. Numerical and analytical studies have been performed of viscous and interacting viscous-inviscid flows with application to 3D boundary layers, wing-body configurations, and internal flow problems. In this area, the development of numerical techniques and analytical tools is of primary significance although the application of these methods to practical problems of interest has also been accomplished. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1980
Accession Number
ADA095817

Entities

People

  • Robert J. Cresci
  • Stanley G. Rubin

Tags

Communities of Interest

  • Advanced Electronics
  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Boundary Layer
  • Boundary Layer Flow
  • Data Acquisition
  • Difference Equations
  • Flow Fields
  • Fluid Dynamics
  • Geometry
  • Heat Transfer
  • Laser Beams
  • Navier Stokes Equations
  • Regions
  • Three Dimensional
  • Turbulent Flow
  • Turbulent Mixing
  • Wind Tunnels
  • Wing Body Configurations

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • Theoretical Analysis.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow