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Calculation of potential flow past airship bodies in yaw (1932)
NASA Technical Reports Server (NTRS) · leaf 33
K.A.C.A, Technical Memorand-am No. 675 Figs. 15,15,17,18 0.4 0.3 J—' Q. ■«^0,2 CO io.i id M 0 -0.1 0 100 200 Fig. It) Jxmction of curve K(x,r,|iP) '^^^ 0.8 0.9 1.0 for x= 50. (Fuhrmaim shape ig. 16 The N(k2) function. Mo.l, 1= 230) … 0 1.0 y 2.0 Eig, 18 Siirface superposition of source - sink "bocly.NASA Technical Reports Server (NTRS)
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