MAT Program Test Summary Report. Biconic Body with Slice/Flap

Abstract

Detailed shock layer surveys, surface heat transfer and pressure, and force and moment data were obtained on sharp and blunted bicone models tested under laminar and turbulent boundary layer flow conditions. The objective of these tests is to obtain basic body of data under hypersonic flow conditions, and under a variety of flow conditions and geometric parameters which would be useful for checking and validating the newly developed parabolized Navier-Stokes (PNS) codes, and other detailed flow field codes.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1982
Accession Number
ADA118242

Entities

People

  • A. Martellucci
  • S. Weinberg

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Boundary Layer
  • Boundary Layer Flow
  • Computational Fluid Dynamics
  • Data Acquisition
  • Flow Fields
  • Flow Visualization
  • Fluid Dynamics
  • Fluid Flow
  • Heat Transfer
  • Measurement
  • Mechanical Properties
  • Physics Laboratories
  • Pressure Distribution
  • Pressure Measurement
  • Test Facilities
  • Turbulent Flow

Fields of Study

  • Physics

Readers

  • Computer Science.
  • Fluid Mechanics and Fluid Dynamics.
  • Pavement Materials Engineering.

Technology Areas

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