ROLE OF CONSTRAINTS IN INVERSE DESIGN FOR TRANSONIC AIRFOILS.

被引：0

作者：

Volpe, G. ^{[1
]}

Melnik, R.E. ^{[1
]}

机构：

[1] Grumman Aerospace Corp, Bethpage,, NY, USA, Grumman Aerospace Corp, Bethpage, NY, USA

来源：

| 1770年 / 22期

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[11] HARMONIC ANALYSIS METHOD FOR UNSTEADY TRANSONIC FLOW AND ITS APPLICATION TO THE FLUTTER OF AIRFOILS.
Ehlers, F.Edward
Weatherill, Warren H.
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[12] BEZIER PRESENTATION OF AIRFOILS.
Boehm, Wolfgang
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[13] INVERSE METHOD WITH GEOMETRIC CONSTRAINTS FOR TRANSONIC AEROFOIL DESIGN
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SLOOFF, JW
BOERSTOEL, JW
KASSIES, A
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN ENGINEERING, 1986, 22 (02) : 327 - 339
[14] Inverse design of transonic airfoils using parallel simultaneous perturbation stochastic approximation
Xing, X.Q. (xqxing@ntu.edu.sg), 1600, American Institute of Aeronautics and Astronautics Inc. (42):
[15] Inverse design of transonic airfoils using parallel simultaneous perturbation stochastic approximation
Xing, XQ
Damodaran, M
JOURNAL OF AIRCRAFT, 2005, 42 (02): : 568 - 570
[16] Dual-point design of transonic airfoils using the hybrid inverse optimization method
Kim, HJ
Rho, OH
JOURNAL OF AIRCRAFT, 1997, 34 (05): : 612 - 618
[17] UNSTEADY POTENTIAL FLOW FOR OSCILLATING AIRFOILS.
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[18] Fast Inverse Design of Transonic Airfoils by Combining Deep Learning and Efficient Global Optimization
Deng, Feng
Yi, Jianmiao
AEROSPACE, 2023, 10 (02)
[19] Inverse design of transonic airfoils using genetic algorithm and a new parametric shape method
Jahangirian, A.
Shahrokhi, A.
INVERSE PROBLEMS IN SCIENCE AND ENGINEERING, 2009, 17 (05) : 681 - 699
[20] Multiobjective optimization design of transonic airfoils with constraints based on Navier-Stokes equations
Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2000, 18 (03): : 350 - 355

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