This report presents the results of field test measurements to define the noise produced on the ground by military, fixed wing aircraft during controlled level flyovers and ground runups. For flight conditions, data are presented in terms of various acoustic measures over the range 200-25,000 feet minimum slant distance to the aircraft. For ground runups, data are presented as a function of angle and distance to the aircraft. All of the data are normalized to standard acoustic reference conditions of 59 deg. F temperature and 70% relative humidity. Noise data are presented in this Volume 3 for the following aircraft: A-7D, E; A-10A; A-37B; F-4C, D, E, F; F-5A, B; F-5E, F; F-15A; F-16A; F-104C, D, G; F-111A, E; F-111D, and F-111F.
Community Noise Exposure Resulting from Aircraft Operations. Volume 3. Acoustic Data on Military Aircraft: Air Force Attack/Fighter Aircraft
1978
764 pages
Report
Keine Angabe
Englisch
Air Transportation , Aeronautics , Noise Pollution & Control , Aircraft noise , Jet engine noise , Military aircraft , Jet fighters , Attack aircraft , Predictions , Measurement , Communities , Tables(Data) , Sound pressure , Noise pollution , A-7 aircraft , A-10A aircraft , A-37A aircraft , F-4 aircraft , F-5 aircraft , F-15A aircraft , F-16A aircraft , F-104 aircraft , F-111 aircraft