Acta Aeronautica et Astronautica Sinica (Selected Articles),

Abstract

Application of adaptive Control to aircraft systems; by Application of rotor induced velocity field of the vortex theory to the study of stability and controllability of a helicopter with hingeless rotor; A second-order theory for three-dimensional unsteady flows and its application to thin wings with attack angle at supersonic and hypersonic speeds.

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Document Details

Document Type
Technical Report
Publication Date
Oct 10, 1986
Accession Number
ADA173610

Entities

People

  • Hongyue Zhang
  • Longde He
  • Shicum Wang
  • Zhiming Xin
  • Zhongji Chen

Organizations

  • National Air and Space Intelligence Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Adaptive Systems
  • Aircrafts
  • Control Systems
  • Control Systems Engineering
  • Delta Wings
  • Dynamic Response
  • Engineering
  • Engineers
  • Frequency
  • Helicopters
  • Mach Number
  • Military Aircraft
  • Standards
  • Stratified Fluids
  • Thin Wings
  • Two Dimensional

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.

Technology Areas

  • Hypersonics