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机译:超声速进气道启动瞬态动力学的实验识别
University of Texas at Austin, Austin, Texas 78712 ,Department of Aerospace Engineering and Engineering Mechanics, 1 University Station C0600;
University of Texas at Austin, Austin, Texas 78712 ,Department of Aerospace Engineering and Engineering Mechanics, 1 University Station C0600;
University of Texas at Austin, Austin, Texas 78712 ,Department of Aerospace Engineering and Engineering Mechanics, 1 University Station C0600;
U.S. Air Force Research Laboratory, Wright-Patterson Air Force Base, Ohio 45433;
Spectral Energies, LLC, Dayton, Ohio 45431;
机译:使用主动和被动涡流发生器控制超音速入口隔离器的启动
机译:超声速进气启动/停止的多重稳定性和复杂路线
机译:边界层对质量注入引起的超声速进气未启动的影响
机译:实验性超音速进气口起步的检测和瞬态动力学建模
机译:马赫数为5的流程中入口/隔离器配置中的启动动力学的实验研究。
机译:经历空间异质性环境的实验人群的瞬时局部适应和源库动态
机译:近等熵超音速入口中的不启动的动态表征和主动控制