Detection of Unsteady Boundary Layer Transition Using Three Experimental Methods (AIAA 2016-1072)
Aerospace sciences meeting
2016-01-01
22 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
High Velocity Path Control of Quadrotors (AIAA 2015-1072)
British Library Conference Proceedings | 2015
|An Experimental Study of Unsteady Separated Shock Wave / Boundary Layer Interactions AIAA Paper
British Library Conference Proceedings | 2007
|AIAA 2006-1072 Towards the Creation of a Physics-Based Ground Effect Model
British Library Conference Proceedings | 2006
|