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.
NASA Aerodynamic Research Applicable to Business Aircraft
Sae Technical Papers
National Business Aircraft Meeting and Engineering Display ; 1971
01.02.1971
Aufsatz (Konferenz)
Englisch
Applicable numerical optimization methods for aerodynamic design of civil aircraft
Online Contents | 2014
|Nasa Aircraft Controls Research, 1983
NTIS | 1984
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