NASA Technical Reports Server (NTRS) 19820003181: A comparison of theoretical and experimental pressure distributions for two advanced fighter wingsReport as inadecuate



 NASA Technical Reports Server (NTRS) 19820003181: A comparison of theoretical and experimental pressure distributions for two advanced fighter wings


NASA Technical Reports Server (NTRS) 19820003181: A comparison of theoretical and experimental pressure distributions for two advanced fighter 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) 19820003181: A comparison of theoretical and experimental pressure distributions for two advanced fighter wings
A comparison was made between experimental pressure distributions measured during testing of the Vought A-7 fighter and the theoretical predictions of four transonic potential flow codes. Isolated wind and three wing-body codes were used for comparison. All comparisons are for transonic Mach numbers and include both attached and separate flows. In

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







Related documents