Pressure drop in tubing in aircraft instrument installations (1937)
NASA Technical Reports Server (NTRS) · leaf 29
Fig. 3 K.A.C.A. Technical Note Ho. 593 ^Oatsiie diameter for 0.035" wall thickness … 0.5 1 2 3 4 5 6 7 89 10 15 20 Air flow at zero altitude, Cubic feet per minute 'figure 3.- Chart for computing the approximate pressure drop in smooth tubing at pressures near 30 inches of mercury.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
