Analysis of unsteady pressure distributions around an NACA 0012 aeroelastic wing-model in transonic flow
Mechanical and Aerospace Engineering
M.S. in Mechanical Engineering
University of Missouri--Rolla
xii, 137 pages
© 1995 Jacopo Frigerio, All rights reserved.
Thesis - Citation
Print OCLC #
Link to Catalog Record
Full-text not available: Request this publication directly from Missouri S&T Library or contact your local library.http://merlin.lib.umsystem.edu/record=b2712518~S5
Frigerio, Jacopo, "Analysis of unsteady pressure distributions around an NACA 0012 aeroelastic wing-model in transonic flow" (1995). Masters Theses. 1483.
Share My Thesis If you are the author of this work and would like to grant permission to make it openly accessible to all, please click the button above.