A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds write by John C. Martin. This book was released on 1954. A Theoretical Investigation of the Aerodynamics of Wing-tail Combinations Performing Time-dependent Motions at Supersonic Speeds available in PDF, EPUB and Kindle. 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
Modeling of longitudinal unsteady aerodynamics of a wingtail combination - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Modeling of longitudinal unsteady aerodynamics of a wingtail combination write by . This book was released on . Modeling of longitudinal unsteady aerodynamics of a wingtail combination available in PDF, EPUB and Kindle.
Technical Note - National Advisory Committee for Aeronautics
Technical Note - National Advisory Committee for Aeronautics - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Technical Note - National Advisory Committee for Aeronautics write by United States. National Advisory Committee for Aeronautics. This book was released on 1956. Technical Note - National Advisory Committee for Aeronautics available in PDF, EPUB and Kindle.
General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations
General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations write by Jack N. Nielsen. This book was released on 1956. General Theory of Wave-drag Reduction for Combinations Employing Quasi-cylindrical Bodies with an Application to Swept-wing and Body Combinations available in PDF, EPUB and Kindle. 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
Report - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Report write by . This book was released on 1957. Report available in PDF, EPUB and Kindle.
