The scaling laws of a Michalke and Michel predict flyover noise of a single stream shock free circular jet from static data or static predictions. The theory is based on a farfield solution to Lighthill's equation and includes density terms which are important for heated jets. This theory is compared with measured data using two static jet noise prediction methods. The comparisons indicate the theory yields good results when the static noise levels are accurately predicted
The results of a test program conducted in the NASA Ames 40- by 80-Foot Wind Tunnel to determine the...
Available experimental data comparing the in-flight and static behavior of fan noise are reviewed. T...
A theory of aerodynamic noise is presented which differs from Lighthill's theory primarily in the wa...
A scaling law is derived for predicting the flyover noise spectra of a single-stream shock-free circ...
A scaling law for the prediction of flyover noise spectra of a single stream shock free circular jet...
Flight simulation experiments were conducted in an anechoic free jet facility over a broad range of ...
Differences between flight data and predictions of jet engine exhaust noise were reconciled by consi...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
A semi-empirical model for predicting the noise generated by jets exhausting from circular nozzles i...
Noise from an unheated sonic jet in the presence of an external flow is measured in a free-jet wind ...
The sound intensity of jet noise in flight is derived in a co-ordinate system fixed to the jet engin...
The noise of the TF30 afterburning turbofan engine in an F-111 airplane was determined from static (...
The acoustic analogy introduced by Lighthill to study jet noise is now over 50 years old. In the pre...
A model scale flight effects test was conducted in the 40 by 80 foot wind tunnel to investigate the ...
Development of good predictive models for jet noise has always been plagued by the difficulty in obt...
The results of a test program conducted in the NASA Ames 40- by 80-Foot Wind Tunnel to determine the...
Available experimental data comparing the in-flight and static behavior of fan noise are reviewed. T...
A theory of aerodynamic noise is presented which differs from Lighthill's theory primarily in the wa...
A scaling law is derived for predicting the flyover noise spectra of a single-stream shock-free circ...
A scaling law for the prediction of flyover noise spectra of a single stream shock free circular jet...
Flight simulation experiments were conducted in an anechoic free jet facility over a broad range of ...
Differences between flight data and predictions of jet engine exhaust noise were reconciled by consi...
High intensity acoustic radiation occurs when turbulence convects past airframe trailing edges. A ma...
A semi-empirical model for predicting the noise generated by jets exhausting from circular nozzles i...
Noise from an unheated sonic jet in the presence of an external flow is measured in a free-jet wind ...
The sound intensity of jet noise in flight is derived in a co-ordinate system fixed to the jet engin...
The noise of the TF30 afterburning turbofan engine in an F-111 airplane was determined from static (...
The acoustic analogy introduced by Lighthill to study jet noise is now over 50 years old. In the pre...
A model scale flight effects test was conducted in the 40 by 80 foot wind tunnel to investigate the ...
Development of good predictive models for jet noise has always been plagued by the difficulty in obt...
The results of a test program conducted in the NASA Ames 40- by 80-Foot Wind Tunnel to determine the...
Available experimental data comparing the in-flight and static behavior of fan noise are reviewed. T...
A theory of aerodynamic noise is presented which differs from Lighthill's theory primarily in the wa...