Design and Wind-Tunnel Analysis of a Fully Adaptive Aircraft Configuration
45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference
2004-01-01
Conference paper
Electronic Resource
English
AIAA-2004-1727 Design and Wind-Tunnel Analysis of a Fully Adaptive Aircraft Configuration
British Library Conference Proceedings | 2004
|WIND TUNNEL TEST RESULTS FOR A CANARD ROTOR/WING AIRCRAFT CONFIGURATION
British Library Conference Proceedings | 2001
|Transonic Wind-Tunnel Flows About a Fully Configured Model of Aircraft (TN)
Online Contents | 1995
|