Sonic Boom Alleviation Using Keel Configurations

Author:

Marconi Frank1,Bowersox Rodney D. W.2,Schetz Joseph A.3

Affiliation:

1. Allied Aerospace Industries, Ronkonkoma, New York 11779

2. Texas A&M University, College Station, Texas 77843

3. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. A low-boom and low-drag design method for supersonic aircraft and its applications on airfoils;Advances in Aerodynamics;2021-09-01

2. Drag and Heat Transfer Effects on Hypersonic Vehicles in Close-Proximity Flight;Journal of Aircraft;2020-09

3. Staged Aft Body for Alleviation of Tail Boom;AIAA Journal;2014-12

4. Flow Disturbance and Surface Roughness Effects on Cross-Flow Boundary-Layer Transition in Supersonic Flows;44th AIAA Fluid Dynamics Conference;2014-06-13

5. Aeronautics and astronautics: Recent progress and future trends;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2009-12-01

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