Aircraft Pay-Offs and Requirements for a Jet Flap Propulsion System

751091

02/01/1975

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
Jet flaps, because of their propulsive lift characteristics, have the theoretical potential to improve fighter aircraft performance. Studies have shown that to achieve these improvements afterburning jet flaps are required. The benefits gained are primarily at high lift coefficients; consequently, there is a significant interaction between the jet flap effects and the wing aerodynamics. In order to integrate the jet flap into fighter designs, short afterburners are necessary. Titanium sandwich construction appears to be the best structural concept for a jet flap.
Meta TagsDetails
DOI
https://doi.org/10.4271/751091
Pages
9
Citation
Silverman, S., "Aircraft Pay-Offs and Requirements for a Jet Flap Propulsion System," SAE Technical Paper 751091, 1975, https://doi.org/10.4271/751091.
Additional Details
Publisher
Published
Feb 1, 1975
Product Code
751091
Content Type
Technical Paper
Language
English