Return to search

Shock interaction due to blunt leading edges of two-dimensional hypersonic inlets.

No description available.
Identiferoai:union.ndltd.org:LACETR/oai:collectionscanada.gc.ca:QMM.49033
Date January 1969
CreatorsO'Connell, Kevin John.
PublisherMcGill University
Source SetsLibrary and Archives Canada ETDs Repository / Centre d'archives des thèses électroniques de Bibliothèque et Archives Canada
LanguageEnglish
Detected LanguageEnglish
TypeElectronic Thesis or Dissertation
Formatapplication/pdf
CoverageMaster of Engineering (Department of Mechanical Engineering)
RightsAll items in eScholarship@McGill are protected by copyright with all rights reserved unless otherwise indicated.
Relationalephsysno: 000470522, proquestno: AAIMK06029, Theses scanned by UMI/ProQuest.

Page generated in 0.0026 seconds