Formulation of Design Envelope Criterion in Terms of Deterministic Spectral Procedure

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.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1990
Accession Number
ADA222120

Entities

People

  • J. G. Jones

Organizations

  • Royal Aircraft Establishment

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aircraft Models
  • Aircrafts
  • Amplitude
  • Coefficients
  • Data Science
  • Dynamic Response
  • Equations
  • Frequency
  • Frequency Response
  • Information Science
  • Linear Systems
  • Models
  • Nonlinear Dynamics
  • Nonlinear Systems
  • Power Spectra
  • Simulations
  • Standards

Readers

  • Approximation Theory.
  • Aviation Science / Aeronautics.
  • Systems Analysis and Design