Sonic Boom Reduction Using an Adjoint Method for Wing- Body Configurations in Supersonic Flow

机译：超声速流中采用翼形构型的伴随方法降低声波动臂

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来源
《9th AIAA/ISSMO Symposium on Multidisciplinary Analysis and Optimization》|2002年|P.1-10|共10页
会议地点 Atlanta GA(US)
作者
S. Nadarajah; A. Jameson; J. Alonso;
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作者单位

Stanford University, Stanford, CA;

Stanford University, Stanford, CA;

Stanford University, Stanford, CA;

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原文格式 PDF
正文语种
中图分类航空、航天技术的研究与探索;
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2. Reduction of the sonic boom level in supersonic aircraft flight by the method of surface cooling [J] . V.M. Fomin, V.F. Chirkashenko, V.F. Volkov, Thermophysics and Aeromechanics . 2013,第6期

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3. Reduction of the sonic boom level by heating the flow in front of the body [J] . A. V. Potapkin, D. Yu. Moskvichev Shock Waves . 2014,第4期

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4. Sonic Boom Reduction Using an Adjoint Method for Wing- Body Configurations in Supersonic Flow [C] . American Institute of Aeronautics and Astronautics/International Society for Structural and Multidisciplinary Optimization Symposium on Multidisciplinary Analysis and Optimization . 2002

机译：Sonic Boom使用超声波流动的翼身配置进行伴随方法
5. Coupled sensitivity analysis by discrete-analytical direct and adjoint methods with applications to aeroelastic optimization and sonic boom minimization. [D] . Nikbay, Melike. 2002

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7. Sonic Boom Reduction Using An Adjoint Method For Wing-Body Configurations In Supersonic Flow [O] . Juan J, Siva K. Nadarajah, Antony Jameson, 2002

机译：在超声速流中采用翼形配置的伴随方法降低声波动臂

Sonic Boom Reduction Using an Adjoint Method for Wing- Body Configurations in Supersonic Flow

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