Read Online An Experimental and Analytical Investigation of the Effect of Spanwise Curvature on Wing Flutter at Mach Number of 0.7 - National Aeronautics and Space Administration file in PDF Online

Full Download An Experimental and Analytical Investigation of the Effect of Spanwise Curvature on Wing Flutter at Mach Number of 0.7 - National Aeronautics and Space Administration | ePub

An experimental and analytical study was conducted at Mach 0.7 to investigate the effects of spanwise curvature on flutter. Two series of rectangular planform wings of aspect ration 1.5 and curvature ranging from zero (uncurved) to 1.04/ft were flutter tested in the NASA Langley Transonic Dynamics Tunnel (TDT). One series consisted of models with a NACA 65 A010 airfoil

Title : An Experimental and Analytical Investigation of the Effect of Spanwise Curvature on Wing Flutter at Mach Number of 0.7
Author : National Aeronautics and Space Administration
Language : en
Rating :
4.90 out of 5 stars
Type : PDF, ePub, Kindle
Uploaded : Apr 07, 2021

Post Your Comments: