Equivalence rule and transonic flow theory involving lift.

AIAA Journal ◽  
1973 ◽  
Vol 11 (8) ◽  
pp. 1210-1212 ◽  
Author(s):  
H. K. CHENG ◽  
M. M. HAFEZ
Keyword(s):  
Transonic Flow ◽  
Flow Theory

Linearized Transonic Flow About Slender Bodies at Zero Angle of Attack

1961 ◽  
Vol 28 (4) ◽  
pp. 481-490 ◽  
Author(s):  
P. F. Maeder ◽  
H. U. Thommen
Keyword(s):  
Shock Waves ◽  
Transonic Flow ◽  
Angle Of Attack ◽  
Flow Theory ◽  
Theoretical Investigations ◽  
Slender Bodies

The simple linearized transonic flow theory as originally proposed by Oswatitsch and Keune [1] and by the present authors [2] is improved by considering and partially correcting its error. In this manner a theory which is easy to apply and which should be valid for a great number of smooth bodies is obtained. This improved theory predicts shock waves in the lower transonic regions. It is applied to a number of significant body and airfoil shapes and its predictions are compared with experiments and results of other theoretical investigations.

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