Airfoil section characteristics as applied to the prediction of air forces and their distribution on wings (1938)
NASA Technical Reports Server (NTRS) · leaf 17
actual pressure differences p are obtained the solution of the force and moment distribution along by multiplying by the dynamic pressure, g= 10.79 the upper wing in the 30-foot-per-second gust, corre- pounds per square foot. These pressures, calculated sponding to design Condition I of reference… … Distonce from L.E., percent c =0.1065. Q 1.125 Figure 14.—Pressure distribution over center section in the accelerated-flight condition. =0.12. BIPLANE The following example is given to illustrate the appli- With the foregoing data, the method of reference 6 cation of the method to biplane problems…
NASA Technical Reports Server (NTRS)
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