Computational Study of High-Angle-of-Attack Missile Flows Using Two-Equation Turbulence Models
36th, Aerospace sciences meeting ; 1998 ; Reno; NV
1998-01-01
ALL
Nos AIAA 98-0001 to 98-1069 with gaps held only
Conference paper
English
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Computational Investigations of Subsonic High Angle of Attack Missile Flows
British Library Conference Proceedings | 1998
|Application of Turbulence Models to Separated High-Angle-of-Attack Flows
British Library Conference Proceedings | 1998
|