Hybrid Wing Body Acoustic Test in the 14 by 22 ft Subsonic Tunnel
NASA Acoustics Technical Working Group Meeting ; 2010 ; Hampton, VA, US
2010-10-21
Miscellaneous
No indication
English
Blended-wing-body subsonic commercial transport
AIAA | 1998
|Blended-Wing-Body Subsonic Commercial Transport
British Library Conference Proceedings | 1998
|Conceptual Design of an N+3 Hybrid Wing Body Subsonic Transport
British Library Conference Proceedings | 2010
|