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sciences naturelles et appliquées - iate.europa.eu

Publications scientifiques

Transition within leeward plane of axisymmetric bodies at incidence in supersonic flow... Transition over four axisymmetric bodies (namely, Sears-Haack body, semi-Sears-Haack body, straight cone and flared cone) with different axial pressure gradients was measured in two different facilities with different unit Reynolds...
général - core.ac.uk - PDF: hdl.handle.net
Computational investigation of supersonic boundary layer transition over canonical fuselage nose configurations... Transition over four axisymmetric bodies (namely, Sears-Haack body, semi-Sears-Haack body, 5-degree straight cone and flared cone) with different axial pressure gradients has been studied at Mach 2 in order to understand the ...
général - core.ac.uk - PDF: hdl.handle.net
Investigation at mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45©� sweptback highly tapered wing in combination with basic and indented bodies /... Data were obtained for the wing in the presence of a basic Sears-Haack body and a body indented symmetrically for a Mach number of 1.2.NACA...
général - core.ac.uk - PDF: www.hathitrust.org
An inverse design method for supersonic airfoils... The robustness of the method is demonstrated through several distinct design cases including supersonic airfoils, unique geometries, and a Sears-Haack body
général - core.ac.uk - PDF: digitalcommons.calpoly.edu
An unstructured wave drag code for preliminary design of future supersonic aircraft... Finally, in order to validate the code, the new code is used to compute the wave-drag of a Sears-Haack body and F-16 and the results are compared to the results from AWAVE, the Harris Wave Drag program
général - core.ac.uk - PDF: citeseerx.ist.psu.edu

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métallurgie et sidérurgie - acta.es


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