Airframe-Propulsion Integration Design and Optimization
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Publisher
IntechOpen
Link
http://www.intechopen.com/download/pdf/66112
Reference21 articles.
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3. Huang W, Wang ZG, Jin L, Liu J. Effect of cavity location on combustion flow field of integrated hypersonic vehicle in near space. Journal of Vision. 2011;14(4):339-351. DOI: 10.1007/s12650-011-0100-3
4. Stevens DR. Practical Considerations in Waverider Applications. AIAA Paper 92-42471992. DOI: 10.2514/6.1992-4247
5. Takashima N, Lewis MJ. Waverider Configurations Based on Nonaxisymmetric Flow Fields for Engine-Airframe Integration. AIAA Paper 94-03801994. DOI: 10.2514/6.1994-380
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