This investigation was carried out to determine the distribution of load over the wings of a high speed airplane under all conditions of flight. In particular it was desired to find the pressure distribution during level flight, over the portions of the wings in the slipstream and, during violent maneuvers, over the entire wing surface. The method used consisted in connecting a number of holes in the surface of the wings to recording multiple manometers mounted in the fuselage of the airplane. In this way simultaneous records could be taken on all of the holes for any desired length of time. (author)
Pressure Distribution over the Wings of an MB-3 Airplane in Flight
01.01.1925
Sonstige
Keine Angabe
Englisch
Pressure distribution over the wings of an MB-3 airplane in flight
Engineering Index Backfile | 1924
|Pressure distribution over wings and tail surfaces of PW-9 pursuit airplane in flight
Engineering Index Backfile | 1930
|Engineering Index Backfile | 1921