Wing Pressure Distributions Over the Lift Range of the Convair XF92A Delta-Wing Airplane at Subsonic and Transonic Speeds Page: 42 of 137
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to UNT Digital Library by the UNT Libraries Government Documents Department.
Extracted Text
The following text was automatically extracted from the image on this page using optical character recognition software:
NACA RM 15507
aL
TABLE VI. - Continued
REASSURE COEFTICIENTS AND AERODYNAMIC CHARACTERISTICS
OF THE CONVAIR XF-92A WNG
[wind-up turn; M = 0.91 to 0o.84(e) M = 0.89
cNA = 0.27a = 6.7 0
BeL = 4.80as
41
Pressure coefficients
Orifice Row A Row B Row C Row D Row E
Upper Lower Upper Lo<er Upper Lower Upper Lower Upper Lower
surface surface surface surface surface surface surface surface surface surface
1 -0.041 ----- -o.462 ----- -0.726 ----- -o.95 ---- -o.642
2 -.401 0.559 -.870 0.284 -.750 0.224 -.870 - -.822 -0.065
3 -.409 .272 -.474 .212 -.702 .163 -.858 0.175 -.65 -.173
4 -.269 .260 -.365 .151 -.606 .135 -.854 .127 -.490 -.517
5 -.257 .200 -.341 ----- -.613 .24 -.738 .079 -.389 -.221
6 -.269 .163 -.317 .139 -.594 -.029 -.758 .060 -.221 -.089
7 -.245 .151 -.305 ----- -.546 -.053 -.678 .043 -.197 -.101
8 -.245 .103 -.517 - -.594 -.113 -.534 -.065
9 -.185 .045 -.341 .o043 -.606 -.088 -.185 -.317
10 -.209 .115 -.377 -.041 -.058 -.096 -.125 -.185
11 -.221 .079 -.437 -.173 .o4 ----- -.o46 -.618
12 -.293 -.041 -.522 -.245 .115 -.69o -.058 -.437
15 -.305 -.029 -.329 -.113 .055 -.570 -.012 -.125
14 -.401 ----- .oo -.o65 .079 .055 .019 .055
15 -.305 -.120 .163-----
16 -.425 -.197 .079 -.101
17 -.498 -.245 .091 .024
18 -----
19 - ----
20 -.125 -.096
21 -.o65 -.449
22 -.005 -.125
23 .067 o
Upcoming Pages
Here’s what’s next.
Search Inside
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Keener, Earl R. & Jordan, Gareth H. Wing Pressure Distributions Over the Lift Range of the Convair XF92A Delta-Wing Airplane at Subsonic and Transonic Speeds, report, November 30, 1955; (https://digital.library.unt.edu/ark:/67531/metadc61544/m1/42/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.