Aeroelastic Problems Associated With External Stories and Innovative Scaling Laws for Such Problems

Abstract

This AASERT grant was initially funded 7/1/95 and a Ph.D. student (Anne Le) was hired and started her studies towards a Ph. D. degree working on the problem of active control of flutter induced by stores on the wing of a typical fighter aircraft and its aeroelastic scaling. The main thrust of her research has been the development of an aeroelastic computer code capable of simulating the subsonic flutter of a fighter type wing, including stores, as well as partial span control surfaces that can be actively controlled and used for flutter suppression.

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Document Details

Document Type
Technical Report
Publication Date
Jun 30, 2000
Accession Number
ADA388304

Entities

People

  • Peretz P. Friedmann

Organizations

  • University of California, Los Angeles

Tags

Communities of Interest

  • Space
  • Weapons Technologies

DTIC Thesaurus Topics

  • Abstracts
  • Air Force
  • Aspect Ratio
  • Control Surfaces
  • Control Systems
  • Engineering
  • External Stores
  • Fighter Aircraft
  • Frequency Domain
  • Scaling Laws
  • Scientific Research
  • Sea Level
  • Students
  • Theses
  • Three Dimensional
  • Time Domain
  • Universities

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Research Science/Academic Research
  • Theoretical Analysis.