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Author : H. Schlichting
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.:/5 (11 download)
Download or read book Calculation of Lift Distribution of Swept Wings written by H. Schlichting and published by . This book was released on 1948 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : H. Schlichting
Publisher :
ISBN 13 :
Total Pages : 131 pages
Book Rating : 4.:/5 (11 download)
Download or read book Note on the Calculation of the Lift Distribution of Swept Wings written by H. Schlichting and published by . This book was released on 1947 with total page 131 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. Air Force. Air Matériel Command
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.:/5 (758 download)
Download or read book The Lift Distribution of Swept-back Wings written by United States. Air Force. Air Matériel Command and published by . This book was released on 1946 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two procedures for calculating the lift distribution along the span are given, in which better account is taken of the distribution of circulation over the area than in the Prandtl lifting-line theory. The methods are also applicable to wings with sweepback. Calculated results according to two methods agree excellently. Using the second, simpler method one needs about 3 hours for the calculation of the lift distribution of a straight wing, and about eight hours for this calculation for the swept-back wing. The results are compared with those of the Multhopp method and with experimental results. Finally there is a brief not on the swept-back wing in sideslip.
Author : Albert P. Martina
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.3/5 (91 download)
Download or read book Method for Calculating the Rolling and Yawing Moments Due to Rolling for Unswept Wings with Or Without Flaps Or Ailerons by Use of Nonlinear Section Lift Data written by Albert P. Martina and published by . This book was released on 1953 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: The methods of NACA Reports 865 and 1090 have been applied to the calculation of the rolling- and yawing-moment coefficients due to rolling for unswept wings with or without flaps or ailerons. The methods allow the use of nonlinear section lift data together with lifting-line theory. Two calculated examples are presented in simplified computing forms in order to illustrate the procedures involved.
Author : J. Weissinger
Publisher :
ISBN 13 :
Total Pages : 51 pages
Book Rating : 4.:/5 (862 download)
Download or read book The Lift Distribution of Swept-back Wings written by J. Weissinger and published by . This book was released on 1947 with total page 51 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two procedures for calculating the lift distribution along the span are given in which a better account is taken of the distribution of circulation over te area than in the Prandtl lifting-line theory. The methods are also applicable to wing sweepback. Calculated results for the two methods were in agreement.
Author : Alex Goodman
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.3/5 (91 download)
Download or read book Estimation of the Damping in Roll of Wings Through the Normal Flight Range of Lift Coefficient written by Alex Goodman and published by . This book was released on 1949 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: The development of three methods for calculating the damping in roll through the normal flight range of lift coefficient for wing plan forms having various sweep angles, aspect ratios, and taper ratios is presented and comparisons between experimental and calculated results are made.
Author : Martin Zlotnick
Publisher :
ISBN 13 :
Total Pages : 40 pages
Book Rating : 4.3/5 (91 download)
Download or read book A Simplified Mathematical Model for Calculating Aerodynamic Loading and Downwash for Midwing Wing-fuselage Combinations with Wings of Arbitrary Plan Form written by Martin Zlotnick and published by . This book was released on 1953 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James C. Sivells
Publisher :
ISBN 13 :
Total Pages : 722 pages
Book Rating : 4.F/5 ( download)
Download or read book Method for Calculating Lift Distribtutions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data written by James C. Sivells and published by . This book was released on 1951 with total page 722 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for calculating lift distributions for unswept wings with flaps or ailerons using nonlinear section lift data. This method is based upon lifting-line theory and is an extension to the method described by NACA Report 865. Simplified computing forms containing detailed examples are given for both symmetrical and asymmetrical lift distributions. A few comparisons of experimental and calculated characteristics are also presented.
Author : Eli Herman Benstein
Publisher :
ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.E/5 ( download)
Download or read book The Spanwise Lift Distribution of Swept Wings at Subsonic Speeds written by Eli Herman Benstein and published by . This book was released on 1952 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Michael J. Mann
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Calculation of the Twist Distribution of Wings Designed for Cruise at Transonic Speeds written by Michael J. Mann and published by . This book was released on 1974 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harvard Lomax
Publisher :
ISBN 13 :
Total Pages : 48 pages
Book Rating : 4.3/5 (91 download)
Download or read book Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms written by Harvard Lomax and published by . This book was released on 1949 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.
Author : James C. Sivells
Publisher :
ISBN 13 :
Total Pages : 70 pages
Book Rating : 4.3/5 (91 download)
Download or read book Method for Calculating Lift Distributions for Unswept Wings with Flaps Or Ailerons by Use of Nonlinear Section Lift Data written by James C. Sivells and published by . This book was released on 1951 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for calculating lift distributions for unswept wings with flaps or ailerons using nonlinear section lift data. This method is based upon lifting-line theory and is an extension to the method described by NACA Report 865. Simplified computing forms containing detailed examples are given for both symmetrical and asymmetrical lift distributions. A few comparisons of experimental and calculated characteristics are also presented.
Author : Robert Thomas Jones
Publisher : Princeton University Press
ISBN 13 : 1400860776
Total Pages : 227 pages
Book Rating : 4.4/5 (8 download)
Download or read book Wing Theory written by Robert Thomas Jones and published by Princeton University Press. This book was released on 2014-07-14 with total page 227 pages. Available in PDF, EPUB and Kindle. Book excerpt: Originator of many of the theories used in modern wing design, Robert T. Jones surveys the aerodynamics of wings from the early theories of lift to modern theoretical developments. This work covers the behavior of wings at both low and high speeds, including the range from very low Reynolds numbers to the determination of minimum drag at supersonic speed. Emphasizing analytical techniques, Wing Theory provides invaluable physical principles and insights for advanced students, professors, and aeronautical engineers, as well as for scientists involved in computational approaches to the subject. This book is based on over forty years of theoretical and practical work performed by the author and other leading researchers in the field of aerodynamics. Originally published in 1990. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author : James C. Sivells
Publisher :
ISBN 13 :
Total Pages : 512 pages
Book Rating : 4.F/5 ( download)
Download or read book Method for Calculating Wing Characteristics by Lifting-line Theory Using Nonlinear Section Life Data written by James C. Sivells and published by . This book was released on 1947 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for calculating wing characteristics by lifting-line theory using nonlinear section lift data. Material from various sources is combined with some original work into the single complete method described.
Author : William Mutterperl
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Calculation of Span Load Distributions on Swept-back Wings written by William Mutterperl and published by . This book was released on 1941 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Span load distributions of swept-back wings have been calculated. The method used was to replace the wing with a bound vortex at the quarter-chord line and to calculate the downwash due to the system of bound and trailing vortices to conform at the three-quarter-chord line to the slope of the flat-plate wing surface. Results are given for constant-chord and 5:1 tapered plan forms, for swee-pback angles of 0, 30 and 45 degresss, and for aspect ratios of 3, 6, and 9. Some comments on the stalling of swept-back wings are included.
Author :
Publisher :
ISBN 13 :
Total Pages : 112 pages
Book Rating : 4.:/5 (317 download)
Download or read book A Finite-step Method for Estimating the Spanwise Lift Distribution of Wings in Symmetric, Yawed, and Rotary Flight at Low Speeds written by and published by . This book was released on 1978 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Harold N. Murrow
Publisher :
ISBN 13 :
Total Pages : 62 pages
Book Rating : 4.:/5 (31 download)
Download or read book An Application of a Numerical Technique to Lifting-surface Theory for Calculation of Unsteady Aerodynamic Forces Due to Continuous Sinusoidal Gusts on Several Wing Planforms at Subsonic Speeds written by Harold N. Murrow and published by . This book was released on 1963 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
