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Aviation History
1917
1917 - 0864.PDF
1/llGHT AtfOTST 33, 1917- Fig. 3. i n rJ ; \ -.v CHARACTERISTIC CURVE FOR LIFT DRIFT OF U.S.A. 7 -o U.S.A. 2|-a -a! o- U.S.A. 3 ~A a! A- U.S.A. 4 —>i *•! *— U.S.A. 5|-*-•-_ »r •*—• p.A.F ei-t frj «— Velocity: 30 U.P.H. Pounds sq.ft. I U.P.H.'finits Density of air: .07608 lbs. / cu.ft. Models: 78 "x 3" ACHUSETTS INSTITUTE \0F TECHNO OOY April 3rd, 1917 S .7 1.0 -2" 0' 4° 6° e° io" Angle of wing chord to wind 12' 14' 16° 78° 20° iifl kfill Tra'ling Edge TRAVEL OF CENTER 0; | FOR U.S.A. 1 PRESSURE U.S.A. 2 U.S.A. 3 U.S.A. 4 U.S.A. 6 R.A.F. 6 _o--» — o! a— Velocity: 30 M.P.H. Density of air: .07808 lbs. j cu.ft.^-^— ; ' Models: 18"x MASSACHUSETTS INSTITUTE\0F TECHNOLOGY •April 4th, 7877 -4' -2' 2' 4C 6J Angle of i 8' -10' g cJigrd to wind 12' W- 76° •ir ~gg? Fig. 4. 864
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