The Lewis Research Center cold-flow model externally blown flap (EBF) noise research test program is summarized. Both engine under-the-wing and over-the-wing EBF wing section configurations were studied. Ten large scale and nineteen small scale EBF models were tested. A limited number of forward airspeed effect and flap noise suppression tests were also run. The key results and conclusions drawn from the flap noise tests are summarized and discussed
A wind tunnel investigation was made of the noise characteristics of a 4.42 m(14.5 foot) semispan, e...
Noise tests were conducted with small-scale models of externally blown-flap powered-lift systems tha...
Noise data with models of both internally and externally blown jet flaps designed for STOL aircraf
Noise tests were conducted with a nozzle exhausting over a small scale model of an externally blown ...
Noise data were obtained with a large-scale cold-flow model of a two-flap, under-the-wing, externall...
Noise data were obtained with a large externally blown flap model. A fan-jet engine exhaust was simu...
The sensitivity of flap interaction noise to variations in engine-under-the-wing externally blown fl...
Noise tests were conducted on a large scale, cold flow model of an engine-under-the-wing externally ...
June 1972Also issued as an M.S. thesis, Massachusetts Institute of Technology, Dept. of Aeronautics ...
Screening tests of upper surface blowing on externally blown flaps configurations were conducted. No...
A summary is given of the noise suppression tests conducted for the STOL aircraft. The tests were ma...
Noise measurements were obtained on models of jet-augmented lift systems which are currently being c...
Small scale model acoustic experiments were conducted to measure the noise produced in the flyover a...
Noise tests were conducted on a small-scale model of an externally blown flap lift augmentation syst...
An interim procedure for predicting externally blown flap (EBF) noise spectra anywhere below a power...
A wind tunnel investigation was made of the noise characteristics of a 4.42 m(14.5 foot) semispan, e...
Noise tests were conducted with small-scale models of externally blown-flap powered-lift systems tha...
Noise data with models of both internally and externally blown jet flaps designed for STOL aircraf
Noise tests were conducted with a nozzle exhausting over a small scale model of an externally blown ...
Noise data were obtained with a large-scale cold-flow model of a two-flap, under-the-wing, externall...
Noise data were obtained with a large externally blown flap model. A fan-jet engine exhaust was simu...
The sensitivity of flap interaction noise to variations in engine-under-the-wing externally blown fl...
Noise tests were conducted on a large scale, cold flow model of an engine-under-the-wing externally ...
June 1972Also issued as an M.S. thesis, Massachusetts Institute of Technology, Dept. of Aeronautics ...
Screening tests of upper surface blowing on externally blown flaps configurations were conducted. No...
A summary is given of the noise suppression tests conducted for the STOL aircraft. The tests were ma...
Noise measurements were obtained on models of jet-augmented lift systems which are currently being c...
Small scale model acoustic experiments were conducted to measure the noise produced in the flyover a...
Noise tests were conducted on a small-scale model of an externally blown flap lift augmentation syst...
An interim procedure for predicting externally blown flap (EBF) noise spectra anywhere below a power...
A wind tunnel investigation was made of the noise characteristics of a 4.42 m(14.5 foot) semispan, e...
Noise tests were conducted with small-scale models of externally blown-flap powered-lift systems tha...
Noise data with models of both internally and externally blown jet flaps designed for STOL aircraf