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Chapter 3: Some Fundamental Aspects of Compressible Flow
This chapter contains 17 unsolved problems.
# Problem Description Online
1 Problem 1
Changes in p, T, ρ 		link
2 Problem 2
Speed of sound in H2, He, and N2 		link
3 Problem 3
Speed of sound in CO2 at different temperatures 		link
4 Problem 4
Changes in ρ, T, V across sound wave 		link
5 Problem 5
Mach number 		link
6 Problem 6
Mach number 		link
7 Problem 7
Speed of airplane at an altitude 		link
8 Problem 8
Supersonic wind tunnel 		link
9 Problem 9
Mach at which the airplane flies 		link
10 Problem 10
Mach number and velocity in wind tunnel 		link
11 Problem 11
Supersonic wind tunnel 		link
12 Problem 12
Mach number and velocity of different gas 		link
13 Problem 13
Air velocity and Mach angle (non-standard units) 		link
14 Problem 14
Mach waves from projectile 		link
15 Problem 15
Mach number of a flying aircraft 		link
16 Problem 16
Aircraft noise distance 		link
17 Problem 17
Speed of a flying aircraft 		link
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