NASA Technical Reports Server (NTRS) 19840020665: Study of transonic flow over swept wingsReport as inadecuate



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


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

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







Related documents