Parametric Investigation of Box Wing Configuration in Viscous Flow Regime (AIAA 2018-3814)
Applied aerodynamics (Conference)
2018-01-01
27 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1918
Gust Loads Calculation of a Flying Wing Configuration (AIAA 2018-3326)
British Library Conference Proceedings | 2018
|AIAA-2003-3814 Vortex Wake Investigation of an Airbus A340 Model Using PIV in a Towing Tank
British Library Conference Proceedings | 2003
|Information hiding using random sequences [3814-04]
British Library Conference Proceedings | 1999
|