NASA Technical Reports Server (NTRS) 19810013486: Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62Report as inadecuate



 NASA Technical Reports Server (NTRS) 19810013486: Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62


NASA Technical Reports Server (NTRS) 19810013486: Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62 - Download this document for free, or read online. Document in PDF available to download.

Download or read this book online for free in PDF: NASA Technical Reports Server (NTRS) 19810013486: Pressure and force data for a flat wing and a warped conical wing having a shockless recompression at Mach 1.62
A conical nonlinear flow computer code was used to design a warped (cambered) wing which would produce a supercritical expansion and shockless recompression of the crossflow at a lift coefficient of 0.457, an angle of attack of 10 deg, and a Mach number of 1.62. This cambered wing and a flat wing the same thickness distribution were tested over a r

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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