Masters Theses
Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack
Department(s)
Mechanical and Aerospace Engineering
Degree Name
M.S. in Aerospace Engineering
Publisher
University of Missouri--Rolla
Publication Date
Spring 1992
Pagination
ix, 113 pages
Rights
© 1992 Deborah Anne Engelmeyer, All rights reserved.
Document Type
Thesis - Citation
File Type
text
Language
English
Thesis Number
T 6351
Print OCLC #
26480312
Recommended Citation
Engelmeyer, Deborah Anne, "Computational study of impulsive and accelerating flow over NACA0015 airfoils at high angles of attack" (1992). Masters Theses. 966.
https://scholarsmine.mst.edu/masters_theses/966
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.
