Some Problems of Modelling Aeroelastic Phenomena in a Transonic Tunnel,

Abstract

The parameters of training jets are usually at the lower limit of the transonic region. The aeroelastic phenomena which are observed are considerably influenced by air compressibility. The theoretical solution of these phenomena does not yield satisfactory results, and there is a need for the use of model systems. This contribution analyzes the capabilities of aeroelastic modelling by a transonic model.

Document Details

Document Type
Technical Report
Publication Date
Jan 22, 1975
Accession Number
ADA007391

Entities

People

  • J. Malecek
  • J. Vrhel

Organizations

  • National Air and Space Intelligence Center

Tags

DTIC Thesaurus Topics

  • Compressive Properties
  • Continents
  • Czechoslovakia
  • Eastern Europe
  • Education
  • Eurasia
  • Europe
  • Geographic Regions
  • Training

Fields of Study

  • Physics

Readers

  • Aerospace Engineering
  • Fluid Dynamics.
  • Theoretical Analysis.