The Zero-Lift Drag of Several Configurations of the XAAM-N-2 Pilotless Aircraft, TED No. NACA DE332 Page: 9 of 20
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CONFIDENTIAL
NACA RM SL50OC6a
* * 8
Q
oPe
* *
' S
0@NOSE COORDINATES
CONFIDENTIAL
TABLE II
i.
*,Fuselage station
Fuselage radius (in.)
(in.) Nose fineness Nose fineness
ratio = 5.00 ratio = 6.25
0 0 0
.066 .113 .141
.110 .225 .281
.185 .450 .563
.251 .675 .844
.367 1.125 1.406
.472 1.575 1.969
.615 2.250 2.813
.789 3.150 3.938
1.027 4.500 5.625
1.226 5.738 7.172
1.698 9.000 11.250
2.260 13.500 16.875
2.513 15.750 19.688
2.750 18.000 22.500
2.973 20.250 25.313
3.182 22.500 28.125
3.378 24.750 30.938
3.562 27.000 33.750
3.632 27.900 34.875
3.733 29.250 36.563
3.891 31.500 39.375
4.167 36.000 45.000
4.381 40.500 50.625
4.500 45.000 56.250
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Hall, James R. & Sandahl, Carl A. The Zero-Lift Drag of Several Configurations of the XAAM-N-2 Pilotless Aircraft, TED No. NACA DE332, report, March 16, 1950; (https://digital.library.unt.edu/ark:/67531/metadc65533/m1/9/: accessed April 18, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.