Effect of circumferential groove casing treatment parameters on axial compressor flow range

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.

Détails bibliographiques
Auteur principal: Hanley, Brian K. (Brian Kyle)
Autres auteurs: Choon S. Tan and Edward M. Greitzer.
Format: Thèse
Langue:eng
Publié: Massachusetts Institute of Technology 2010
Sujets:
Accès en ligne:http://hdl.handle.net/1721.1/59675
Description
Résumé:Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2010.