Numerical analyses of discrete gust response for an aircraft

Guowei Yang, Shigeru Obayashi

Research output: Contribution to journalArticle

35 Citations (Scopus)

Abstract

Based on Navier-Stokes equations and structural and flight dynamic equations of motion, dynamic responses in vertical discrete gust flow perturbation are investigated for a supersonic transport model. A tightly coupled method was developed by subiterations between aerodynamic equations and dynamic equations of motion. First, under the assumption of rigid-body and single freedom of motion in the vertical plunging, the results of a direct-coupling method are compared with the results of quasi-steady model method. Then, gust responses for the one-minus-cosine gust profile are analyzed with two freedoms of motion in plunging and pitching for the airplane configurations with and without the consideration of structural deformation.

Original languageEnglish
Pages (from-to)1353-1359
Number of pages7
JournalJournal of Aircraft
Volume41
Issue number6
DOIs
Publication statusPublished - 2004

ASJC Scopus subject areas

  • Aerospace Engineering

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