50 Ma, = 1 i 0 = 0, max 40 30 Maj→ 00 Maz > 1 Ma, < 1 20 Weak Strong 10 10 /5 3. 1.5 1.2 10 20 30 50 60 70 80 90 ß, degrees 0, degrees

Refrigeration and Air Conditioning Technology (MindTap Course List)
8th Edition
ISBN:9781305578296
Author:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Publisher:John Tomczyk, Eugene Silberstein, Bill Whitman, Bill Johnson
Chapter42: Heat Gains And Heat Losses In Structures
Section: Chapter Questions
Problem 10RQ: If the R-value of a construction material is 2.0, what isits U-value? A. 0.25 B. 0 50 C. 1.0 D. 2.0
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Consider supersonic airflow approaching the nose of a two-dimensional wedge at a Mach number of 3. Using Fig. , determine the minimum shock angle and the maximum deflection angle a straight oblique shock can have.

50
Ma, = 1
i 0 = 0,
max
40
30
Maj→ 00
Maz > 1
Ma, < 1
20
Weak
Strong
10
10 /5
3.
1.5
1.2
10
20
30
50
60
70 80
90
ß, degrees
0, degrees
Transcribed Image Text:50 Ma, = 1 i 0 = 0, max 40 30 Maj→ 00 Maz > 1 Ma, < 1 20 Weak Strong 10 10 /5 3. 1.5 1.2 10 20 30 50 60 70 80 90 ß, degrees 0, degrees
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