Doctoral Dissertations

New acceleration potential method for supersonic unsteady aerodynamics of lifting surfaces, further extension of the nonplanar supersonic doublet point method, and nonlinear, nongradient optimized rational function approximations for supersonic, transient response unsteady aerodynamics

Author

Ashish Tewari

Department(s)

Mechanical and Aerospace Engineering

Degree Name

Ph. D. in Aerospace Engineering

Publisher

University of Missouri--Rolla

Publication Date

Spring 1992

Pagination

xiii, 157 pages

Rights

© 1992 Ashish Tewari, All rights reserved.

Document Type

Dissertation - Citation

File Type

text

Language

English

Thesis Number

T 6418

Print OCLC #

26981087

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