Numerical solutions to two problems in fluid mechanics. Part I, Part II, Leading edge separation from a yawed sleder delta wing. Rarefied leading edge flow of a diatomic gas
Author(s)
Pullin, Dale Ian
Type
Thesis
Version
Open Access
Date Issued
1974
Date Awarded
1974
Copyright Statement
Attribution NoDerivatives 4.0 International Licence (CC BY-ND)
Creator
Pullin, Dale Ian
Publisher Department
Department of Aeronautical Engineering
Publisher Institution
Imperial College London
Qualification Level
Doctoral
Qualification Name
Doctor of Philosophy (PhD)
Author Permission
Not granted
