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

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=b2112531~S5

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