Accession Number : AD0699371

Title :   HELICOPTER EXTERNAL SLING SYSTEM BASIC VIBRATION DATA.

Descriptive Note : Engineering rept.,

Corporate Author : ARMY TRANSPORTATION ENGINEERING AGENCY FORT EUSTIS VA

Personal Author(s) : Cottingham,George M.

Report Date : DEC 1969

Pagination or Media Count : 11

Abstract : Simulated tests were conducted of helicopter externally slung loads ranging from 2,000 to 4,000 pounds on an analog computer. (Author)

Descriptors :   (*CARGO, AIRBORNE), (*HELICOPTERS, SUSPENSION DEVICES), FASTENINGS, LOADS(FORCES), SHOCK(MECHANICS), VIBRATION, RESONANCE, COMPUTER PROGRAMMING, SIMULATION

Subject Categories : Helicopters
      Couplers, Fasteners, and Joints

Distribution Statement : APPROVED FOR PUBLIC RELEASE