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NASA Aerodynamic Research Applicable to Business Aircraft
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English
Abstract
A review is made of NASA aerodynamic research of interest to the designer of business aircraft. The results of wind-tunnel and flight studies of several current aircraft are summarized. The attainment of STOL performance is discussed and the effectiveness of several lift augmentation concepts is examined. Finally, the potentialities and problems of flight at and beyond the speed of sound are discussed.
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Loftin, L. and McKinney, M., "NASA Aerodynamic Research Applicable to Business Aircraft," SAE Technical Paper 710378, 1971, https://doi.org/10.4271/710378.Also In
References
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