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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1994, Vol. 15 ›› Issue (1): 46-49.

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DEVELOPMENT AND APPLICATION OF AIRPLANK AIRLOAD CALCULATION SOFTWARE IN ACCORDANCE WITH NATIONAL MILITARY SPECIFICATION

Cheng Gang   

  1. Box 72 of Xi′an,Xi′an,710089
  • Received:1992-12-24 Revised:1993-07-13 Online:1994-01-25 Published:1994-01-25

Abstract: The paper introduces the difficulties met in A/C loads calculation during abrupt pitching maneuver and rolling pullout, and in wing load calculation during rolling maneuvers. It also provides relevant Solutions and development status of software in accordance with national military specification《Military airplane strength and rigidity specification》

Key words: aerodynamicloads, pitchfinchiration, roll, aircraft maneuvers

CLC Number: