Results of measurement in maneuvering flight analyzed and found to verify fact that knowledge of tail load parameters will permit calculation of horizontal tail load; critical conditions for design enumerated.
Flight measurements of aerodynamic loads on horizontal tail surface of fighter-type airplane
Nat Advisory Commitee Aeronautics -- Tech Note
1947
55 pages
Report
Englisch
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Flight studies of horizontal-tail loads experienced by fighter airplane in abrupt maneuvers
Engineering Index Backfile | 1944