Using CFD Solutions as Inputs of Sonic Boom Propagation Calculation
Author:
Publisher
Springer Singapore
Link
http://link.springer.com/content/pdf/10.1007/978-981-13-3305-7_12
Reference8 articles.
1. Farhat C, Maute K, Argrow B et al (2002) A shape optimization methodology for reducing the sonic boom initial pressure rise. In: Proceedings of the 40th AIAA aerospace sciences meeting and exhibit. AIAA Paper No. 2002-145
2. Sasaki D, Obayashi S (2003) Low-boom design optimization for SST canard-wing-fuselage configuration. In: Proceedings of the 16th AIAA computational fluid dynamics conference. AIAA Paper No. 2003-3432
3. Page JA, Plotkin KJ (1991) An efficient method for incorporating computational fluid dynamics into sonic boom prediction. In: Proceedings of the AIAA 9th applied aerodynamics conference. AIAA Paper No. 91-3275
4. George A (1968) Reduction of sonic boom by azimuthal redistribution of overpressure. AIAA Paper No. 68-159
5. Plotkin KJ, Page JA (2002) Extrapolation of sonic boom signatures from CFD solutions. In: Proceedings of the 40th AIAA aerospace sciences meeting and exhibit. AIAA Paper No. 2002-0922
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