Consider quasi-one-dimensional isentropic flow of a perfect gas through a variable-area channel. The relationship between the March number M and the flow area A, derived by Zucrow and Hoffman (1976) is given by: (r+1)/2(y-1) 2 (1+ A Mly +1 A 1 Where A* is the choking area (i.e. the area where M-1) and y is the specific heat ratio of the flowing gas. For each value of ɛ, two values of M exist, one less than 1 (i.e. subsonic flow) and one exceeding 1 (i.e. supersonic flow). Calculate both values of M for e=10.0 and y-1.4 by Newton_Raphson method. For the supersonic root, take Mo=5.0. For the subsonic root, take Mo-D0.2.
Consider quasi-one-dimensional isentropic flow of a perfect gas through a variable-area channel. The relationship between the March number M and the flow area A, derived by Zucrow and Hoffman (1976) is given by: (r+1)/2(y-1) 2 (1+ A Mly +1 A 1 Where A* is the choking area (i.e. the area where M-1) and y is the specific heat ratio of the flowing gas. For each value of ɛ, two values of M exist, one less than 1 (i.e. subsonic flow) and one exceeding 1 (i.e. supersonic flow). Calculate both values of M for e=10.0 and y-1.4 by Newton_Raphson method. For the supersonic root, take Mo=5.0. For the subsonic root, take Mo-D0.2.
Functions and Change: A Modeling Approach to College Algebra (MindTap Course List)
6th Edition
ISBN:9781337111348
Author:Bruce Crauder, Benny Evans, Alan Noell
Publisher:Bruce Crauder, Benny Evans, Alan Noell
ChapterA: Appendix
SectionA.2: Geometric Constructions
Problem 10P: A soda can has a volume of 25 cubic inches. Let x denote its radius and h its height, both in...
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