Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack
Mechanical and Aerospace Engineering
M.S. in Aerospace Engineering
University of Missouri--Rolla
ix, 113 pages
© 1992 Deborah Anne Engelmeyer, All rights reserved.
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Full-text not available: Request this publication directly from Missouri S&T Library or contact your local library.http://laurel.lso.missouri.edu/record=b2112531~S5
Engelmeyer, Deborah Anne, "Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack" (1992). Masters Theses. 966.
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