Flight tests were conducted in a CV-990 jet transport with engines at idle power to investigate aircraft airframe noise. Test results showed that airframe noise was measured for the aircraft in the landing configuration. The results agreed well with the expected variation with the fifth power of velocity. For the aircraft in the clean configuraton, it was concluded that airframe noise was measured only at higher airspeeds with engine idle noise present at lower speeds. The data show that landing gear and flaps make a significant contribution to airframe noise
Laboratory experiments were conducted to provide information on quantifying the annoyance response o...
Ground noise level prediction and measurements during climbout operations of jet transport aircraf
Noise measurement evaluations of various takeoff-climbout profiles of four engine turbojet transport...
Flyover measurements of the airframe noise produced by the AeroCommander, JetStar, CV-990, and B-747...
Airframe noise measurements are reported for the DC-9-31 aircraft flown at several speeds and with a...
Variation in engine noise for two landing approach configurations of jet transport aircraf
A delayed flap approach procedure was flight tested using the NASA CV-990 airplane to measure and an...
A series of flyover noise measurements have been accomplished utilizing a large jet transport aircra...
Climbout and landing approach noise measurements for three engine turbofan transport aircraf
To establish a realistic lower limit for the noise level of advanced supersonic transport aircraft w...
An exploratory study of airframe noise on a small-scale model of a supersonic transport concept was ...
The results of baseline noise flight tests are presented. Data are given for a point 1.85 kilometers...
A critical assessment of the state of the art in airframe noise is presented. Full-scale data on the...
Calculated values of airframe noise levels corresponding to FAA noise certification conditions for s...
A semiempirical maximum overall sound pressure level (OASPL) airframe noise model was derived. Noise...
Laboratory experiments were conducted to provide information on quantifying the annoyance response o...
Ground noise level prediction and measurements during climbout operations of jet transport aircraf
Noise measurement evaluations of various takeoff-climbout profiles of four engine turbojet transport...
Flyover measurements of the airframe noise produced by the AeroCommander, JetStar, CV-990, and B-747...
Airframe noise measurements are reported for the DC-9-31 aircraft flown at several speeds and with a...
Variation in engine noise for two landing approach configurations of jet transport aircraf
A delayed flap approach procedure was flight tested using the NASA CV-990 airplane to measure and an...
A series of flyover noise measurements have been accomplished utilizing a large jet transport aircra...
Climbout and landing approach noise measurements for three engine turbofan transport aircraf
To establish a realistic lower limit for the noise level of advanced supersonic transport aircraft w...
An exploratory study of airframe noise on a small-scale model of a supersonic transport concept was ...
The results of baseline noise flight tests are presented. Data are given for a point 1.85 kilometers...
A critical assessment of the state of the art in airframe noise is presented. Full-scale data on the...
Calculated values of airframe noise levels corresponding to FAA noise certification conditions for s...
A semiempirical maximum overall sound pressure level (OASPL) airframe noise model was derived. Noise...
Laboratory experiments were conducted to provide information on quantifying the annoyance response o...
Ground noise level prediction and measurements during climbout operations of jet transport aircraf
Noise measurement evaluations of various takeoff-climbout profiles of four engine turbojet transport...