Computational Analysis of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack
43rd AIAA Aerospace Sciences Meeting and Exhibit
01.01.2005
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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
|