The Transonic Jet Flap-A Review of Recent Results

751089

02/01/1975

Event
Aerospace Engineering and Manufacturing Meeting
Authors Abstract
Content
Experimental results are used to explore the physical mechanism of lift augmentation and the drag due to lift, and to show the inadequacies of the Taylor-Spence thin jet model of the jet flap. In the jet-flapped wing-fuselage configuration, 3D effects, particularly due to the wing-fuselage interference, are shown to have major effects on the performance of the jet flap. At large sweeps the 3D vortical nature of the shock-induced separation is shown to also play a dominant role.
Meta TagsDetails
DOI
https://doi.org/10.4271/751089
Pages
9
Citation
Yoshihara, H., and Zonars, D., "The Transonic Jet Flap-A Review of Recent Results," SAE Technical Paper 751089, 1975, https://doi.org/10.4271/751089.
Additional Details
Publisher
Published
Feb 1, 1975
Product Code
751089
Content Type
Technical Paper
Language
English