Design and qualification of a supersonic wind tunnel for...

Proceedings of the Institution of Mechanical Engineers Part G Journal of Aerospace Engineering 2015 / 03 Vol. 229; Iss. 3

Design and qualification of a supersonic wind tunnel for induced boundary layer transition research

Bottini, H., Paniagua, G., Schreivogel, P., Sonda, A., de las Heras, S.
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Volume:
229
Language:
english
Journal:
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
DOI:
10.1177/0954410014537612
Date:
March, 2015
File:
PDF, 1.42 MB
english, 2015
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