Accession Number:

AD0255752

Title:

MANEUVER LOAD DATA FROM C-130 AIRCRAFT

Descriptive Note:

Corporate Author:

AERONAUTICAL SYSTEMS DIV WRIGHT-PATTERSON AFB OH FLIGHT CONTROL LAB

Personal Author(s):

• PHILLIPS, LAWRENCE

Report Date:

1961-03-01

Pagination or Media Count:

35.0

Abstract:

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.

Descriptors:

• *TRANSPORT AIRCRAFT
• AIR
• DYNAMICS
• ESTIMATES
• FATIGUE
• FATIGUE(MECHANICS)
• FLIGHT
• FLIGHT LOADS
• FLIGHT TESTING
• INDEX TERMS
• LABORATORIES
• LOAD DISTRIBUTION
• LOADS(FORCES)
• MANEUVERABILITY
• MANEUVERS
• MECHANICS
• MISSIONS
• REPORTS
• STANDARDS
• STRUCTURAL PROPERTIES
• STRUCTURES
• VEHICLES

Subject Categories:

• Transport Aircraft

Distribution Statement:

APPROVED FOR PUBLIC RELEASE