Flight Tests on U.S.S. Los Angeles. Part I : Full Scale Pressure Distribution Investigation (1930)
NASA Technical Reports Server (NTRS) · leaf 31
30 REPORT NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS 50 60 70 80 30 100 /I0 120 130 140 Distance from nose, ft Figure 30.—Pressure distribution on hull. Steady turn—rudder 9° 42' port. Run No. 4B—timing line 2 … 50 60 70 80 90 100 110 120 130 140 Distance from noset ft. Figure 31.—Pressure distribution on hull. Steady turn—rudder 8° 18' starboard. Run No. 4C—timing line 7
NASA Technical Reports Server (NTRS)
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