Unsteady Aerodynamics with Applications to Flight Mechanics

Abstract

Unsteady airload measurements have been made on a series of low aspects ratio delta wings subjected to transient pitch motions. These data have been qualified and discussed in several publication which are listed. In addition a discussion on the relevance of unsteady transient airloads to flight mechanics is included. Keywords: Unsteady aerodynamics: Delta wing flows.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1989
Accession Number
ADA211944

Entities

People

  • Holt Ashley

Organizations

  • Stanford University

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautics
  • Air Force
  • Aircrafts
  • Airframes
  • Aspect Ratio
  • Computational Fluid Dynamics
  • Flight Paths
  • Flow Visualization
  • Fluid Dynamics
  • High Angles
  • Leading Edges
  • Measurement
  • Mechanics
  • Steady Flow
  • Steady State
  • Unsteady Aerodynamics
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Structural Health Monitoring of Composite Structures.
  • Systems Analysis and Design