Study of the Influence of Aircraft Geometry on the Computed Flowfield During Thrust Reversers Operation
25th, Aerodynamic measurement technology and ground testing conference ; 2006 ; San Francisco, CA
Aerodynamic measurement technology and ground testing conference ; AIAA Paper 2006-3673
2006-01-01
AIAA Paper 2006-3673
Including 25th AIAA aerodynamic measurement technology and ground testing conference 24th AIAA applied aerodynamics conference; 3rd AIAA flow control conference; 36th AIAA fluid dynamics conference and exhibit; 37th AIAA plasmadynamics and lasers conference; 9th AIAA/ASME joint thermophysics and heat transfer conference.; Paper numbers 2006-2805 to 2006-3925 with gaps held. Held on CD-ROM.; Shelved in Conference Index - see disc 11 for papers from the 25th Aerodynamic measurement technology and ground testing conference
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
THRUST REVERSERS FOR JET AIRCRAFT
SAE Technical Papers | 1957
|Thrust Reversers for Civil STOL Aircraft
SAE Technical Papers | 1973
|Thrust reversers for jet aircraft
Engineering Index Backfile | 1957
|NTRS | 2018
|