Calibration Models for Dynamic Stability Tests

Abstract

This report describes three calibration models in the AGARD series. Model G: A slender wing. Suitable for tests over a wide speed range. Fitted with a fin and a sting fairing. Model H: A thin tapered wing suitable for high speed tests. Model J: A 10 degree semi-angle cone, suitable for high supersonic speed testing.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0676576

Entities

People

  • H. C. Garner
  • R. Fail

Organizations

  • AGARD

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Aircrafts
  • Aspect Ratio
  • Boundary Layer
  • Boundary Layer Transition
  • Calibration
  • Dynamic Tests
  • Layers
  • Measurement
  • Mechanics
  • Model Tests
  • Nato
  • Planform
  • Standards
  • Swept Wings
  • Trailing Edges
  • Transitions

Readers

  • Aerodynamics/Aeronautics.
  • Computational Modeling and Simulation

Technology Areas

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