Computational Analysis of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack
43rd AIAA Aerospace Sciences Meeting and Exhibit
2005-01-01
Conference paper
Electronic Resource
English
Computational Analysis of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack
British Library Conference Proceedings | 2005
|Laminar boundary layer on cone in supersonic flow at large angle of attack
Engineering Index Backfile | 1953
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