飞机非线性飞行载荷计算方法研究

ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2002, Vol. 23 ›› Issue (4): 317-320.

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CALCULATION METHOD ABOUT NONLINEAR FLIGHT LOADS OF AIRCRAFT

DENG Li-dong¹, LI Tian¹, XUE Xiao-chun²

1. Shenyang Institute of Aircraft Design & Research, Shenyang 110035, China;2. Aircraft Design and Research Institute, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

Received:2001-04-27 Revised:2002-03-22 Online:2002-08-25 Published:2002-08-25

Abstract

Abstract:

For implementing the Strength and Stiffness Spoecification of Military Aircraft of China, a set of analysis and calculation methods for aircraft flight loads is presented, which uses nonlinear aerodynamic data of wind tunnel test. Based on the specification, a set of software with flight loads database for nonlinear flight loads analysis is developed successfully. The software has been used for flight loads calculation of F×× aircraft.

Key words: aerodynamic load, inertial load, flight envelope, load envelope

DENG Li-dong;LI Tian;XUE Xiao-chun. CALCULATION METHOD ABOUT NONLINEAR FLIGHT LOADS OF AIRCRAFT[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2002, 23(4): 317-320.

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CALCULATION METHOD ABOUT NONLINEAR FLIGHT LOADS OF AIRCRAFT

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