This content is not included in
your SAE MOBILUS subscription, or you are not logged in.
Effect of Exhaust Deflectors on the Design of Lift Plus Lift/Cruise V/STOL Aircraft
Annotation ability available
Sector:
Language:
English
Abstract
Design and experimental studies are reviewed which demonstrate the effect of vectored nozzle type, shape, location and orientation on V/STOL aircraft design and performance. Single and twin engine aircraft differences are discussed. Complete aircraft sizing and mission results are displayed for twin engine aircraft.
Authors
Citation
Migdal, D., "Effect of Exhaust Deflectors on the Design of Lift Plus Lift/Cruise V/STOL Aircraft," SAE Technical Paper 730959, 1973, https://doi.org/10.4271/730959.Also In
References
- Wooler et al “V/STOL Aircraft Aerodynamic Prediction Methods Investigation.” AFFDL TR 72-26 Jan 1972
- Migdal, D et al “Design Considerations for Supersonic V/STOL Aircraft,” ASME Paper 73-GT-65 April 1973
- Higgins, C et al “Exhaust Jet Wake and Thrust Characteristics of Several Nozzles Designed for VTOL Downwash Suppression.” NASA CR-373 1966