On the Design of Lifting Airfoils with High Critical Mach Number Using Full Potential Theory

We wish to construct airfoils that have the highest free-stream Mach number for a given set of geometric constraints for which the flow is nowhere supersonic. Nonlifting airfoils that maximize the critical Mach number for a given cross-sectional area are known to possess long sonic segments at their...

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Veröffentlicht in:	Theoretical and computational fluid dynamics 1997-02, Vol.9 (1), p.17-32
1. Verfasser:	Kropinski, MCA
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Airfoils Computational fluid dynamics Construction Cross sections Hoisting Mach number Potential theory Sonics Theory
Online-Zugang:	Volltext
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