Effect of Exhaust Deflectors on the Design of Lift Plus Lift/Cruise V/STOL Aircraft 730959
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.
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. Download Citation
Author(s):
David Migdal
Pages: 10
Event:
National Aerospace Engineering and Manufacturing Meeting
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Aircraft
Nozzles
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