Download or read book Some Comparative Calculations with the Lifting Surface Theory of Laschka for Circular and Elliptic Wings Oscillating in Subsonic Flow written by R. J. Zwaan and published by . This book was released on 1964 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NASA Technical Note written by and published by . This book was released on 1969 with total page 936 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1965 with total page 328 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Development of Three dimensional Pressure distribution Functions for Lifting Surfaces with Trailing edge Controls Based on the Integral Equation for Subsonic Flow written by Alfredo Navarro Crespo and published by . This book was released on 1969 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: Three dimensional pressure distribution functions for lifting surfaces with trailing-edge controls based on integral equations for subsonic flow.

Download or read book Report written by and published by . This book was released on 1965 with total page 672 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book AGARD Report written by and published by . This book was released on with total page 462 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1966 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Boundary value problems in diffraction theory and lifting surfa written by Johannes Boersma and published by . This book was released on 1964 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Journal of the Royal Aeronautical Society written by and published by . This book was released on 1965 with total page 1032 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Index Aeronauticus written by and published by . This book was released on 1965 with total page 1316 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book NLR TN W written by Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands) and published by . This book was released on 1964 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Compositio Mathematica written by and published by . This book was released on 1965 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Verslagen en verhandelingen written by Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands) and published by . This book was released on 1970 with total page 164 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Calculation of Lifting Forces on Oscillating Wings written by Valter J. E. Stark and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Steady Subsonic Lifting Surface Theory for Wings with Swept Partial Span Trailing Edge Control Surface written by Richard T. Medan and published by . This book was released on 1973 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Method for Calculating the Aerodynamic Loading on an Oscillating Finite Wing in Subsonic and Sonic Flow written by Harry L. Runyan and published by . This book was released on 1957 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents a method for determing the air forces on an oscillating finite wing of general plan form in subsonic flow including the limiting case of sonic flow. The method utilizing some of the concepts developed by Falkner (British R. & M. No. 1910) for steady lifting-surface theory. The loading on the wing is assumed to be given by a series containing unknown coefficients which satisfies various boundary conditions at the edges. The required integrations are performed by approximate means, and a set of simultaneous equations in terms of the coefficients in the loading series is obtained. The method is applied to rectangular and delta wings and comparison is made with existing theory. A sample calculation is given in an appendix.

Download or read book The Theory of Thin Wings in Subsonic Flow written by Sergeǐ Mikhaǐlovich Belotserkovskiǐ and published by Springer. This book was released on 2013-12-11 with total page 236 pages. Available in PDF, EPUB and Kindle. Book excerpt: