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 4 for the following aircraft: F-100C, D, F; F-101B, C, F; F-102A; F-105B, D, F, G; F-106A, B; T-33A; T-37B; T-38A; T-39A, B, F; T-43A; and U-2.
Community Noise Exposure Resulting from Aircraft Operations. Volume 4. Acoustic Data on Air Force Trainer/Fighter Aircraft
1978
644 pages
Report
Keine Angabe
Englisch
Air Transportation , Aeronautics , Noise Pollution & Control , Aircraft noise , Jet engine noise , Military aircraft , Training planes , Jet fighters , Predictions , Measurement , Communities , Tables(Data) , Sound pressure , Flight testing , Noise pollution , F-100 aircraft , F-101 aircraft , F-102A aircraft , F-105 aircraft , F-106 aircraft , T-33A aircraft , T-37B aircraft , T-38A aircraft , T-39 aircraft , T-43A aircraft , U-2 aircraft