Accession Number:

ADA169946

Title:

Gust Load Prediction and Alleviation on a Fighter Aircraft,

Descriptive Note:

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (FRANCE)

Personal Author(s):

Report Date:

1986-06-01

Pagination or Media Count:

24.0

Abstract:

This paper discusses the influence of turbulence induced dynamic loads on the structural design of fighter aircraft. Methods for calculating dynamic response are given, and the problems associated with improved ride are considered.

Subject Categories:

  • Flight Control and Instrumentation
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE