Vibration and Acoustic Environment of AH-1G Helicopter
Abstract
Vibration and acoustic measurements were made on an AH-1G Helicopter equipped with 7.62 millimeter machine guns, a 40-millimeter grenade launcher, and 7-tube and 19-tube, 2.75-inch rocket launchers to determine the vibration and acoustic environment throughout the helicopter. Tape recordings from 96 accelerometers and 12 microphones were made during various flight conditions and during armament fire. Spectrum analyses were conducted to determine vibratory double amplitude (DA), acceleration, power spectral density (PSD), and sound pressure levels (SPL) versus frequency. Amplitude probability density (APD) plots also are included. Measured vibration and acoustic data are compared with military standards and specification requirements.
Document Details
- Document Type
- Technical Report
- Publication Date
- Apr 01, 1975
- Accession Number
- ADB004205
Entities
People
- Phyllis G. Bolds
- Virgil C. Mcintosh
Organizations
- Flight Dynamics Laboratory