A package of computer programs was developed for analyzing acoustic data from an aircraft flyover. The package assumes the aircraft is flying at constant altitude and constant velocity in a fixed attitude over a linear array of ground microphones. Aircraft position is provided by radar and an option exists for including the effects of the aircraft's rigid-body attitude relative to the flight path. Time synchronization between radar and acoustic recording stations permits ensemble averaging techniques to be applied to the acoustic data thereby increasing the statistical accuracy of the acoustic results. Measured layered meteorological data obtained during the flyovers are used to compute propagation effects through the atmosphere. Final resu...
A detailed analysis of signal processing concerns for measuring aircraft flyover noise is presented....
Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft ...
Wind tunnel study of levels and spectra of pressure fluctuations acting on leeward side of straight ...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
The en route noise test was designed to characterize propagation of propfan noise from cruise altitu...
Coherent demodulation in single and double side bands with frequency modulation telemetry system
A modular computer program (ANOPP) for predicting aircraft flyover and sideline noise was developed....
An assessment of the basic acoustic characteristics and noise reduction potential of an upper surfac...
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
A theoretical propagation model that represents the scattering properties of an inhomogeneous rain o...
Ground clutter interference is a major problem for airborne pulse Doppler radar operating at low alt...
Results are presented of acoustic tests performed on an STS payload shroud simulator to determine th...
Effect of turbulence and shear flow on launch vehicle response and validity of Taylor hypothesis for...
The atmospheric turbulence involved in the fan noise generation is evaluated with an existing model ...
A general purpose computer program was developed for the prediction of vehicle interior noise. This ...
A detailed analysis of signal processing concerns for measuring aircraft flyover noise is presented....
Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft ...
Wind tunnel study of levels and spectra of pressure fluctuations acting on leeward side of straight ...
The feasibility of classifying an airport terminal area for multipath effects, i.e., fadeout potenti...
The en route noise test was designed to characterize propagation of propfan noise from cruise altitu...
Coherent demodulation in single and double side bands with frequency modulation telemetry system
A modular computer program (ANOPP) for predicting aircraft flyover and sideline noise was developed....
An assessment of the basic acoustic characteristics and noise reduction potential of an upper surfac...
Ultrahigh frequency air traffic control satellite simulation experiment using high altitude balloon
A theoretical propagation model that represents the scattering properties of an inhomogeneous rain o...
Ground clutter interference is a major problem for airborne pulse Doppler radar operating at low alt...
Results are presented of acoustic tests performed on an STS payload shroud simulator to determine th...
Effect of turbulence and shear flow on launch vehicle response and validity of Taylor hypothesis for...
The atmospheric turbulence involved in the fan noise generation is evaluated with an existing model ...
A general purpose computer program was developed for the prediction of vehicle interior noise. This ...
A detailed analysis of signal processing concerns for measuring aircraft flyover noise is presented....
Prediction of airframe noise radiation from the landing gear and wheel wells of commercial aircraft ...
Wind tunnel study of levels and spectra of pressure fluctuations acting on leeward side of straight ...