The Transonic Jet Flap-A Review of Recent Results
751089
02/01/1975
- Event
- 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.
- 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.