Effects of varying the relative vertical position of wing and fuselage . .1550 .387 of .+*, :XSiZ JD JH - ° - - - - - C. ,7 , - 3C3—« ,741. 94. p . TABLE D. TABLE VICase E. Angle ofattack JD Jll .Ingle of cT °D- c M - .0734 — P °, -, 234 . 0747 - .0197 .063 — 6,0 .0232 .066 - .032 .0175 .084 -4,5 . 058 ? .0310 .090 - .
Effects of varying the relative vertical position of wing and fuselage . .1550 .387 of .+*, :XSiZ JD JH - ° - - - - - C. ,7 , - 3C3—« ,741. 94. p . TABLE D. TABLE VICase E. Angle ofattack JD Jll .Ingle of cT °D- c M - .0734 — P °, -, 234 . 0747 - .0197 .063 — 6,0 .0232 .066 - .032 .0175 .084 -4,5 . 058 ? .0310 .090 - .134 .0173 .105 - .158 .0214 .113 - .234 .0185 .130 - , 358 .0330 .136 - .336 .0223 .154 - . 354 .0268 ,156 .457 ,0261 .175 ? .453 .0315 .181 .548 . 0335 .20? .557 .0383 .311 .650 ,0420 .230 .557 .0474 .232 .750 .0535 .254 .754 .0575 . 356 .950 .0796 .310 .943 .0843 .312 .1110 ,351 1. 108 .1160 .347 .1540 .363, . 1530 .360 600 *---86 H**- 514 a cii__:.2iv_r_nasa_techdoc_19930080888. 5
Size: 3384px × 739px
Photo credit: © The Reading Room / Alamy / Afripics
License: Licensed
Model Released: No
Keywords: ., bookcentury1900, bookdecade1920, bookidnasatechdoc1, bookyear1921
