A study of methods to increase the lift of supersonic airfoils at low speeds
This thesis presents a study of the problem of improving the lift characteristics of a supersonic wing at low speeds. Trailing edge split flaps, nose flaps, and boundary layer control were investigated singularly and together using the optimum configuration of each. Results indicate that the nose...
Internet
https://thesis.library.caltech.edu/4877/1/Pollock_ad_1947.pdfPollock, Albert David and Reck, Floyd Francis (1947) A study of methods to increase the lift of supersonic airfoils at low speeds. Engineer's thesis, California Institute of Technology. doi:10.7907/J3NG-DD26. https://resolver.caltech.edu/CaltechETD:etd-12082008-083805 <https://resolver.caltech.edu/CaltechETD:etd-12082008-083805>