The Effect of Reduction Gearing on Propeller-body Interference as Shown by Full-Scale Wind-Tunnel Tests (1931)
NASA Technical Reports Server (NTRS) · leaf 8
THE EFFECT OF REDUCTION GEARING ON PROPELLER-BODY INTERFERENCE |c 3g" >! Figure 3.—Open cockpit fuselage with direct-drive J-5 engine Note.—With geared engine, nose was pointed and propeller was l\h inches farther forward
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
