Applications Of Von Karmans Integral Method In Supersonic Wing Theory

Author : Chieh-Chien Chang
Publisher :
ISBN 13 :
Total Pages : 78 pages
Book Rating : 4.75/5 ( download)

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Download or read book Applications of Von Karman's Integral Method in Supersonic Wing Theory written by Chieh-Chien Chang and published by . This book was released on 1951 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: The theory is also applied to find the downwash distribution in the plane of the wing on which the pressure distribution is preassigned. A number of examples are given.

Author : G. N. Ward
Publisher : Cambridge University Press
ISBN 13 : 1316601897
Total Pages : 261 pages
Book Rating : 4.91/5 ( download)

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Download or read book Linearized Theory of Steady High-Speed Flow written by G. N. Ward and published by Cambridge University Press. This book was released on 2016-02-25 with total page 261 pages. Available in PDF, EPUB and Kindle. Book excerpt: Originally published in 1955, this book is devoted exclusively to the problems involved in solving the non-linear equations of motion for compressible fluids.

Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 436 pages
Book Rating : 4.99/5 ( download)

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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 1951 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Johns Hopkins University. Applied Physics Laboratory
Publisher :
ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.95/5 ( download)

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Download or read book Handbook of Supersonic Aerodynamics written by Johns Hopkins University. Applied Physics Laboratory and published by . This book was released on 1957 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 498 pages
Book Rating : 4.93/5 ( download)

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Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1952 with total page 498 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author :
Publisher :
ISBN 13 :
Total Pages : 750 pages
Book Rating : 4.85/5 ( download)

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Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Max A. Heaslet
Publisher :
ISBN 13 :
Total Pages : 656 pages
Book Rating : 4.38/5 ( download)

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Download or read book The Application of Green's Theorem to the Solution of Boundary-value Problems in Linearized Supersonic Wing Theory written by Max A. Heaslet and published by . This book was released on 1949 with total page 656 pages. Available in PDF, EPUB and Kindle. Book excerpt: Under the assumptions of linearized theory, general methods of solutin are given for two- and three-dimensional steady-state and two-dimensional unsteady-state equations of compressible flow. The solutions depend in all cases on the use of Green's equivalent layer of sources, sinks, and doublets. Emphasis is placed on applications in supersonic wing theory, the singularities arising in the integrations being treated by Hadamard's finite part of the technique. Four examples of different character are discussed. In particular, the load distribution over a specific swept-back lifting surface is determined at a free-stream Mach number of one.

Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 162 pages
Book Rating : 4.99/5 ( download)

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Download or read book List of Technical Notes, 1947-1953 written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Author : Maxwell Alfred Heaslet
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.27/5 ( download)

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Download or read book The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms written by Maxwell Alfred Heaslet and published by . This book was released on 1948 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.

Author :
Publisher :
ISBN 13 :
Total Pages : 486 pages
Book Rating : 4.79/5 ( download)

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Download or read book Bibliography of Technical Reports written by and published by . This book was released on 1951 with total page 486 pages. Available in PDF, EPUB and Kindle. Book excerpt: