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Applications Of Von Karmans Integral Method In Supersonic Wing Theory
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Book Synopsis Applications of Von Karman's Integral Method in Supersonic Wing Theory by : Chieh-Chien Chang
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.
Book Synopsis Linearized Theory of Steady High-Speed Flow by : G. N. Ward
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.
Book Synopsis linearized theory of steady high-speed flow by :
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:
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 and published by . This book was released on 1951 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Handbook of Supersonic Aerodynamics by : Johns Hopkins University. Applied Physics Laboratory
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:
Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics
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:
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :
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:
Book Synopsis The Application of Green's Theorem to the Solution of Boundary-value Problems in Linearized Supersonic Wing Theory by : Max A. Heaslet
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.
Book Synopsis Supersonic Lift and Pitiching Moment in Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration by : Frank S. Malvestuto
Download or read book Supersonic Lift and Pitiching Moment in Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration written by Frank S. Malvestuto and published by . This book was released on 1951 with total page 842 pages. Available in PDF, EPUB and Kindle. Book excerpt: Design curves are presented which permit rapid estimations of lift and pitching moment for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Book Synopsis List of Technical Notes, 1947-1953 by : United States. National Advisory Committee for Aeronautics
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:
Book Synopsis The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms by : Maxwell Alfred Heaslet
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.
Book Synopsis Bibliography of Technical Reports by :
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:
Book Synopsis Aeronautical Engineering Review by :
Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1956 with total page 1182 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Volterra's Solution of the Wave Equation as Applied to Three-dimensional Supersonic Airfoil Problems by : Max A. Heaslet
Download or read book Volterra's Solution of the Wave Equation as Applied to Three-dimensional Supersonic Airfoil Problems written by Max A. Heaslet and published by . This book was released on 1947 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt: A surface integral is developed which yields solutions of the linearized partial differential equation for supersonic flow. These solutions satisfy boundary conditions arising in wing theory. Particular applications of this general method are made, using acceleration potentials, to flat surfaces and to uniformlyy loaded lifting surfaces. Rectangular and trapezoidal plan forms are considered along with triangular forms adaptable to swept-forward and swept-back wings. The case of the trangular plan form in sideslip is also included. Emphasis is placed on the systematic application of the method to the lifting surfaces considered and on the possibility of further application.
Book Synopsis The Potential Theory of Unsteady Supersonic Flow by : John Wilder Miles
Download or read book The Potential Theory of Unsteady Supersonic Flow written by John Wilder Miles and published by . This book was released on 1980 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Current Papers by : Aeronautical Research Council (Great Britain)
Download or read book Current Papers written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1956 with total page 664 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Studies by : Zbiginew Krzywoblocki
Download or read book Aerodynamic Studies written by Zbiginew Krzywoblocki and published by . This book was released on 1957 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: