NASA Technical Reports Server (NTRS) 19840020665: Study of transonic flow over swept wingsReportar como inadecuado



 NASA Technical Reports Server (NTRS) 19840020665: Study of transonic flow over swept wings


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The design of shockless airfoils that are appropriate for experimental work on a supersonic transport with an oblique wing are examined. A series of computer codes for the design and analysis of airfoils and wings in two dimensional and three dimensional transonic flow are studied. The oblique wing 3-D code was the forerunner of the later swept win

Autor: NASA Technical Reports Server (NTRS)

Fuente: https://archive.org/







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