Investigation of Temperature Factor Influence on Control Surface Effectiveness in Hypersonic Flows with Moderate Interacation.

Abstract

This report results from a contract tasking Central Aerohydrodynamics Institute as follows: The present report contains the description of the wind tunnel, the model, the test program, and the test results obtained.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1994
Accession Number
ADA339502

Entities

People

  • Yu Eermak

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Boundary Layer
  • Coefficients
  • Control Surfaces
  • Dynamic Pressure
  • Flow
  • Flow Visualization
  • Fluid Dynamics
  • Gas Flow
  • Hypersonic Flow
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Measurement
  • Surfaces
  • Test Equipment
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Dynamics.
  • Technical Research and Report Writing.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow