Download or read book The Drag of Source Distributions in Linearized Supersonic Flow written by C. N. Ward and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Drag of Source Distributions in Linearized Supersonic Flow written by College of Aeronautics and published by . This book was released on 1955 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Drag of Source Distributions in Linearized Supersonic Flow written by G. N. Ward and published by . This book was released on 1955 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Linearized Supersonic Flow written by Wallace Dean Hayes and published by . This book was released on 1947 with total page 348 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Analytic Methods in Aircraft Aerodynamics written by and published by . This book was released on 1970 with total page 758 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Minimum drag Ducted and Closed Three point Body of Revolution Based on Linearized Supersonic Theory written by Hermon M. Parker and published by . This book was released on 1956 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of the three-point body of revolution that has minimum wave drag, based on linearized supersonic-flow theory, has been solved formally without resort to slender-body approximations. The evaluation of the source-distribution function, as well as the body shape, requires numerical procedures. Complete calculations are made for the special case of a closed body with a given section (the third point) at the mid-body position. The existence of a corner at the third point is found to be characteristic of a linear-theory solution of the minimum-drag three-point problem. The conclusion is reached that the influence between the forward end rearward portions of a closed body results in a small increase in the radii of the minimum-drag shape.

Download or read book The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment written by Robert T. Jones and published by . This book was released on 1950 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of the minimum induced drag of wings having a given lift and a given span is extended to include cases in which the bending moment to be supported by the wing is also given. Expressions for the spanwise load distribution and the minimum drag in terms of the lateral position of the load centroid are given. The results show a 15-percent reduction of the induced drag with a 15-percent increase in span over that for an elliptic loading having the same total lift and bending moment.

Download or read book A Higher Order Panel Method for Linearized Supersonic Flow written by F. Edward Ehlers and published by . This book was released on 1979 with total page 260 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Technical Note National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 878 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wing Theory written by A. Robinson and published by Cambridge University Press. This book was released on 2013-09-12 with total page 583 pages. Available in PDF, EPUB and Kindle. Book excerpt: First published in 1956 as part of the Cambridge Aeronautical Series, this book addresses the vital science of wing theory. Robinson and Laurmann record the historic developments in wing theory, including the work of Joukowski and Bernoulli, and discuss developments in supersonic flow and unsteady aerofoil theory. This book will be of value to anyone with an interest in the history of the science of flight.

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1972 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book linearized theory of steady high speed flow written by and published by CUP Archive. This book was released on with total page 268 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1976-02 with total page 1046 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Impingement of Cloud Droplets on a Cylinder and Procedure for Measuring Liquid water Content and Droplet Sizes in Supercooled Clouds by Rotating Multicylinder Method written by E. R. G. Eckert and published by . This book was released on 1955 with total page 330 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Theoretical Investigation of the Drag of Generalized Aircraft Configurations in Supersonic Flow written by E. W. Graham and published by . This book was released on 1957 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt: The basic singularities such as sources, dipoles, lifting elements and volume elements are discussed, and some of the useful inter-relations between these elements are presented. Hayes' method of drag evaluation is derived in detail starting with the general momentum theorem.

Download or read book Sonic Boom Research written by A. R. Seebass and published by . This book was released on 1967 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Report written by College of Aeronautics (Cranfield, Bedfordshire) and published by . This book was released on 1960 with total page 602 pages. Available in PDF, EPUB and Kindle. Book excerpt: