## Theory of wing sections: including a summary of airfoil dataConcise compilation of subsonic aerodynamic characteristics of NACA wing sections, plus description of theory. 350 pages of tables. |

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#### Review: Theory of Wing Sections: Including a Summary of Airfoil Data

User Review - Abdulhaq Elhouderi - GoodreadsThe airfoil data of this book is useless because of the UIUC airfoil data. Read full review

### Contents

THE SIGNIFICANCE OF WINGSECTION CHARACTERISTICS | 1 |

SIMPLE TWODIMENSIONAL FLOWS | 31 |

THEORY OF WING SECTIONS OF FINITE THICKNESS | 46 |

Copyright | |

11 other sections not shown

### Common terms and phrases

16 Section angle aerodynamic center airfoil chord airfoil sections angle of attack angle of zero aspect ratio Basic Thickness Form boundary layer calculated camber cent c NACA cent of airfoil component of velocity corresponding critical Mach design lift coefficient drag coefficient equation f radius th flap deflected 60 fluid increase L.E. ra dius laminar flow leading edge lift-curve slope load distribution Lower surface Station Mach number maximum lift coefficient mean line NACA airfoil normal-force obtained Ordinate Station Ordinate ordinates given percent of chord pitching-moment coefficient position pressure distribution radius th rough Reynolds number Section lift coefficient shown in Fig skin friction slotted flaps Standard roughness Station Ordinate Station Stations and ordinates surface Lower surface surface Station Ordinate theory thickness distribution thickness ratio trailing edge Upper surface Lower v/vy v/V variation velocity distribution wind tunnel Wing Section Continued zero lift