Effect on Drag of Longitudinal Positioning of Half-Submerged and Pylon-Mounted Douglas Aircraft Stores on a Fuselage with and without Cavities between Mach Numbers 0.9 and 1.8 Page: 16 of 46
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NACA RM L54E26
TABLE I. - MODELS TESTED
15
3f
VModel Description t/c of pylon X/L
A Store + pylon 0.10 0.40
B Store + pylon .06 .525
C Store + pylon .06 .6
D Store + pylon + cavity .06 .40
E Store + pylon + cavity .06 .525
F Store + pylon + cavity .06 .65
G Half-submerged store ---- .40
H Half-submerged store - -- .525
I Half-submerged store ---- .65
J Cavity ---- 40
K Cavity ---- .525.
L Cavity 65----
M Store + pylon + cavity .10 .40
N Isolated store ----
0 Fuselage alone ----a I,
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Hoffman, Sherwood & Wolff, Austin L. Effect on Drag of Longitudinal Positioning of Half-Submerged and Pylon-Mounted Douglas Aircraft Stores on a Fuselage with and without Cavities between Mach Numbers 0.9 and 1.8, report, July 15, 1954; (https://digital.library.unt.edu/ark:/67531/metadc64117/m1/16/: accessed April 25, 2024), University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu; crediting UNT Libraries Government Documents Department.