Accession Number:

ADA222120

Title:

Formulation of Design Envelope Criterion in Terms of Deterministic Spectral Procedure

Descriptive Note:

Technical memo.

Corporate Author:

ROYAL AEROSPACE ESTABLISHMENT FARNBOROUGH (UNITED KINGDOM)

Personal Author(s):

Report Date:

1990-01-01

Pagination or Media Count:

15.0

Abstract:

An existing Design Envelope approach to meeting aircraft limit-load requirements for flight in continuous turbulence, using power-spectral methods, is reformulated in a manner which makes no distinction between linear and nonlinear aircraft response. Computational techniques for implementing the new procedure in applications to nonlinear aircraft are discussed and compared with existing simulation methods. Keywords Power spectrum Limit load Turbulence Great Britain.

Subject Categories:

  • Aerodynamics
  • Military Aircraft Operations

Distribution Statement:

APPROVED FOR PUBLIC RELEASE