Pressure measurements made on right upper wing extended to include portions affected by slip stream, fuselage, and windshield, left lower wing, and tail surfaces of Boeing PW-9 airplane, simultaneously with accelerometer readings at center of gravity, wing tip and tail in maneuvers; report is for purpose of making this collection of airplane-load data available to those interested in airplane structures.
Pressure distribution over wings and tail surfaces of PW-9 pursuit airplane in flight
Nat. Advisory Committee Aeronautics -- Report
1930
103 pages
103 Figs.
Report
Englisch
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Pressure distribution on the tail surfaces of pw-9 pursuit airplane in flight
Engineering Index Backfile | 1930
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