Accession Number:

ADA025114

Title:

Measurement of the Static Influence Coefficient of the AH-1G Cobra Fuselage

Descriptive Note:

Preliminary rept. 1 Feb 1975-30 Jan 1976

Corporate Author:

ROCK ISLAND ARSENAL IL GENERAL THOMAS J RODMAN LAB

Report Date:

1976-02-01

Pagination or Media Count:

685.0

Abstract:

An AH-1G Cobra Helicopter minus the tailsection was mounted in a vertical position by personnel at the Ware Simulation Center, Rock Island Arsenal, and the response of the fuselage to various applied loads was then measured. The response, measured as deflections in the direction of applied load, will be used by Bell Helicopter Company for the validation of their NASTRAN math model of the Cobra Helicopter. Initial results of the test indicate good agreement between the experimentally measured deflections and the math model predicted deflections.

Subject Categories:

  • Helicopters

Distribution Statement:

APPROVED FOR PUBLIC RELEASE