Acoustic loads measured on jet-powered STOL configurations are presented for externally blown and upper surface blown flap models ranging in size from a small laboratory model up to a full-scale aircraft model. The implications of the measured loads for potential acoustic fatigue and cabin noise are discussed. Noise transmission characteristics of light aircraft structures are presented. The relative importance of noise transmission paths, such as fuselage sidewall and primary structure, is estimated. Acceleration responses of a historic building and a residential home are presented for flyover noise from subsonic and supersonic aircraft. Possible effects on occupant comfort are assessed. The results from these three examples show that aircraft noise can induce structural responses that are large enough to require consideration in the design or operation of the aircraft.
Effects of aircraft noise on flight and ground structures
01.01.1976
Aufsatz (Konferenz)
Keine Angabe
Englisch
Ground effects on aircraft noise
NTRS | 1979
|Ground Effects on Aircraft Noise
NTIS | 1979
|Ground Effects For Aircraft Noise Certification
AIAA | 2017
|