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A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds

1954 Aerodynamics, Supersonic
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Release : 1954
Genre : Aerodynamics, Supersonic
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Book Synopsis A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds by : John C. Martin

Download or read book A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds written by John C. Martin. This book was released on 1954. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical investigation is presented of the contribution of horizontal tails to the lift and pitching moment due to angle of attack, a constant rate of pitch, and a constant vertical acceleration. Numerical values of the aerodynamic coefficients associated with these motions are presented for a number of two-dimensional wing-tail combinations, a triangular wing-tail combination, and a number of rectangular-wing - triangular-tail combinations.

Modeling of longitudinal unsteady aerodynamics of a wingtail combination

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Book Rating : 788/5 ( reviews)

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Book Synopsis Modeling of longitudinal unsteady aerodynamics of a wingtail combination by :

Download or read book Modeling of longitudinal unsteady aerodynamics of a wingtail combination written by . This book was released on . Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note - National Advisory Committee for Aeronautics

1956 Aeronautics
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Release : 1956
Genre : Aeronautics
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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics. This book was released on 1956. Available in PDF, EPUB and Kindle. Book excerpt:

General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations

1956 Airplanes
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Release : 1956
Genre : Airplanes
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Book Synopsis General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations by : Jack N. Nielsen

Download or read book General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations written by Jack N. Nielsen. This book was released on 1956. Available in PDF, EPUB and Kindle. Book excerpt: The wing-body interference theory of NACA TN 2677 applied to symmetrical wings in combination with quasi-cylindrical bodies permits the direct calculation of pressure-distribution changes produced by body shape changes. This theory is used to determine the relative magnitued of the wave-drag reduction produced by changes in cylinder cross-sectional area and that produced changes in cross-sectional shape (without change in area). The body distortion is expressed as a Fourier series, and an integral equation is derived for the body shape for minimum drag for each Fourier component. Thus the wave-drag reductions for the various Fourier harmonics are independent and additive.

Report

1957 Aeronautics
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Release : 1957
Genre : Aeronautics
Kind : eBook
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Book Synopsis Report by :

Download or read book Report written by . This book was released on 1957. Available in PDF, EPUB and Kindle. Book excerpt:

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