Accession Number:

AD0669875

Title:

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),

Descriptive Note:

Corporate Author:

MINISTRY OF TECHNOLOGY LONDON (ENGLAND) TECHNICAL INFORMATION AND LIBRARY SERVICES

Personal Author(s):

Report Date:

1968-01-01

Pagination or Media Count:

17.0

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

Subject Categories:

  • Aerodynamics
  • Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE