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MANEUVER LOAD DATA FROM C-130 AIRCRAFT
AERONAUTICAL SYSTEMS DIV WRIGHT-PATTERSON AFB OH FLIGHT CONTROL LAB
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Flight Dynamics Lab., Wright Air Development Div., Wright-Patterson Air Force Base, Ohio. MANEUVER LOAD DATA FROM C-130 AIRCRAFT, by Lawrence Phillips. Rept. for Structural Design Criteria. Mar 61, 17p. incl. illus. tables. Proj. 1367 WADD TN 61-44Unclassified report DESCRIPTORS Maneuverability, Transport planes, Flight testing, Structures, Load distribution, Fatigue Mechanics, Design. Open-ended Terms C-130. Structural flight load data are presented from C-130A and B aircraft performing normal operations and analyses of the data. This information is intended for use in determining design criteria for future flight vehicles and in estimating the effect of these missions on a structure of this type in terms of structural fatigue and estimated life.
APPROVED FOR PUBLIC RELEASE