Mathematical description of nonstationary aerodynamic characteristics of a passenger aircraft model in longitudinal motion at large angles of attack

被引：0

作者：

V. I. Petoshin

E. A. Chasovnikov

机构：

[1] Chaplygin Siberian Research Institute of Aviation,

来源：

Journal of Applied Mechanics and Technical Physics | 2011年 / 52卷

关键词：

aircraft model; harmonic vibrations; frequency characteristics; mathematical model;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Aerodynamic loads in problems of flight dynamics of passenger aircraft in stalled flow regimes are described using a mathematical model that includes an ordinary linear first-order differential equation. A procedure for determining the parameters of the mathematical model is proposed which is based on approximating experimental frequency characteristics with the frequency characteristics of the linearized mathematical model. The mathematical model was verified by tests of a modern passenger aircraft model in a wind tunnel.

引用

页码：390 / 396

页数：6

共 17 条

[1] Mathematical description of nonstationary aerodynamic characteristics of a passenger aircraft model in longitudinal motion at large angles of attack
Petoshin, V. I.
Chasovnikov, E. A.
JOURNAL OF APPLIED MECHANICS AND TECHNICAL PHYSICS, 2011, 52 (03) : 390 - 396
[2] Aerodynamic characteristics for a passenger aircraft model with harmonic oscillations on rolling and yawing angles at high angles of attack
Petoshin, V. I.
Chasovnikov, E. A.
THERMOPHYSICS AND AEROMECHANICS, 2013, 20 (01) : 39 - 48
[3] Aerodynamic characteristics for a passenger aircraft model with harmonic oscillations on rolling and yawing angles at high angles of attack
V. I. Petoshin
E. A. Chasovnikov
Thermophysics and Aeromechanics, 2013, 20 : 39 - 48
[4] MATHEMATICAL-MODEL OF AIRCRAFT FOR STUDIES OF NONSTATIONARY AERODYNAMIC CHARACTERISTICS
BELOTSERKOVSKII, SM
PRIKLADNAYA MATEMATIKA I MEKHANIKA, 1975, 39 (05): : 934 - 941
[5] Aerodynamic characteristics of passenger and transport aircraft models at harmonic oscillations on the pitch angle for high angles of attack
Petoshin, V. I.
Chasovnikov, E. A.
THERMOPHYSICS AND AEROMECHANICS, 2011, 18 (03) : 359 - 368
[6] Aerodynamic characteristics of passenger and transport aircraft models at harmonic oscillations on the pitch angle for high angles of attack
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Thermophysics and Aeromechanics, 2011, 18 : 359 - 368
[7] A Method to Improve the Aircraft Aerodynamic Characteristics at High Angles of Attack and in Spin
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Gorbunov V.G.
Efremov A.A.
Drach D.K.
Podobedov V.A.
Russian Aeronautics, 2019, 62 (04): : 604 - 611
[8] Primal research of the effect of flow turbulence on aerodynamic characteristics of a aircraft model at high angles of attack
Li, Feng
Bai, Cun-Ru
Zhou, Wei
Zhang, Chong-Zhong
An, Long
Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics, 2006, 20 (03): : 45 - 47
[9] An Improved Nonlinear Aerodynamic Derivative Model of Aircraft at High Angles of Attack
Mi Baigang
Yu Jingyi
INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2021, 2021
[10] STATE-SPACE REPRESENTATION OF AERODYNAMIC CHARACTERISTICS OF AN AIRCRAFT AT HIGH ANGLES OF ATTACK
GOMAN, M
KHRABROV, A
JOURNAL OF AIRCRAFT, 1994, 31 (05): : 1109 - 1115

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