CALCULATION METHOD FOR THE REACTION OF A GUST OF WIND ON A THIN WING OF ARBITRARY PLANFORM (METOD RASCHETA VOZDEISTVIYAR PORIVA NA PROIZVOLNOE TONKOE KRILO),

Abstract

An ideal incompressible medium is assumed. The method applies to a periodic motion of the wing, arbitrary deformations, entry into a gust, effect of weak blast, etc. It is also applicable to annular wings and composite wing systems. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1968
Accession Number
AD0669875

Entities

People

  • S. M. Belotserkovskii

Tags

DTIC Thesaurus Topics

  • Aircraft Wings
  • Airfoils
  • Airframes
  • Composite Materials
  • Composite Wings
  • Mechanical Structure
  • Ring Wings
  • Thin Wings

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Information Retrieval
  • Structural Dynamics.