Quantcast Figures -11970007

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FIGURES
Page
1
Miramar Layout Showing Thermocouple Locations ..................
12
2
El Toro Layout Showing Thermocouple Locations ..................
13
3
Miramar No. 2 and El Toro Augmenter
Cross-Sections Showing Rake Locations ........................
14
4
Patuxent River Layout Showing Thermocouple
Locations ....................................................
15
5
Dallas Layout Showing Thermocouple Locations ...................
16
6
Augmenter Mass Flow Correlation
with Engine Centered and Aligned .............................
21
7
Augmenter Mass Flow Correlation for
J-79 Engine and J-79 Powered F-4 .............................
22
8
Augmenter Mass Flow Correlation with Significant
Engine Centerline Offset and Misalignment ....................
23
9
Cell Depression Versus Primary Inlet
Flow Rate for Various Facilities .............................
26
10
Cell Depression Versus Primary Inlet Specific
Mass Flow Rate for Various Facilities ........................
27
11
Enclosure Interior Velocity Versus Primary
Mass Flow Rate for Various Facilities ........................
28
12
Enclosure Interior Velocity Versus Primary
Inlet Specific Mass Flow Rate for Various
Facilities ..................................................
29
13
Enclosure Interior Velocity versus Door
Outlet Specific Mass Flow Rate ...............................
30
14
El Toro Internal Flow Patterns
with the A-6 Aircraft ........................................
31
15
Patuxent River Internal Flow Patterns
with the S-3A Aircraft .......................................
32
16
Cherry Point Engine Test Cell Internal Flow
Patterns with the Pegasus Engine .............................
33
17
Augmenter Wall Temperature Distributions for Various
Facilities with Centered and Aligned Engine ....................
35
18
Augmenter Wall Temperature Distributions for Various Facilities
with J-79 Powered F-4 (Single Engine Operation) ..............
36
19
Augmenter Wall Temperature Distribution for Various Facilities
Showing the Effect of Significant Engine Centerline Lateral
Offset and Misalignment (Single Engine Operation) ............
37
20
Augmenter Sidewall Temperature Distribution for F-14A Operation
with One Engine in A/B AT Various Degrees of Aircraft
Misalignment (Sidewall Nearest Operating Engine) .............
39
21
Maximum Augmenter Wall Temperature Parameter for
Various Facilities Showing the Effect of Engine
Centerline Lateral Offset and Misalignment (Single Engine) ...
40
22
Axial Location of Maximum Augmenter Wall Temperature in
Various Facilities for Aligned and Intentionally Misaligned
Aircraft .....................................................
41
23
Miramar and El Toro Augmenter Exit Velocity Distributions ......
43
24
NAS Dallals Engine Test Cell Augmenter Exit Velocity
Distributions ................................................
44
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