The Aeronautical Laboratory of the Stockholm Technical Institute (1935)
NASA Technical Reports Server (NTRS) · leaf 22
Figs. 14,15,16 N.A.C.A. Technical Memorandum No. 766 fag-m fS 96^ 97 r. Dynamic rressure in free jet. .(in mm, alcohol column pressure 0.812) ICO cm from throat, n = 725 r.p.m. Figure 14.-Contour of throat. … Figure 15.-Contour of throat. A— n = 1000 r.p.m. v = 49.5 m/s 0—n = '?25 r.p.m. v = 35 m/s Figure 16.-Excess static pressure along center Cj 40 80 12C 16C 200| line of jot. Entrance cone Exit cone cm
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