Simultaneous visualization of surface and flow field for a projectile

Author:

Ukai Takahiro,Kikuchi Takamasa,Ohtani Kiyonobu,Obayashi Shigeru

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Condensed Matter Physics

Reference17 articles.

1. Bock OH (1974) Focused shadowgraph visualization of boundary-layer transition in aeroballistic range studies. Opt Eng 13(2):143–146. doi: 10.1117/12.7971688

2. Boissevain AG, Interieri PF (1961) Determination of stability derivatives from ballistic range test of rolling aircraft models. NASA technical memorandum X-399

3. Brown JD et al (2006) Complex-trajectory aerodynamics data for code validation from a new free-flight facility. In: Proceedings of the 44th AIAA aerospace sciences meeting and exhibit, AIAA, p 4650

4. Callagban JG (1966) A feasibility investigation concerning the simulation of sonic boom by ballistic models. NASA contractor report, NASA CR-603

5. Canning TN et al (1970) Ballistic-range technology, AGARDograph No. 138, pp 197–266

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