Boundary layer transition measurements in hypervelocity flows in a shock tunnel

---

Autoria(s): Mee, D. J.

Data(s)	01/01/2001
Identificador	http://espace.library.uq.edu.au/view/UQ:96123
Publicador	American Institute of Aeronautics and Astronautics
Palavras-Chave	#EX #290299 Aerospace Engineering not elsewhere classified #780102 Physical sciences
Tipo	Conference Paper