Reducing either thrust or climb airspeed results in reduced sound-pressure levels. Reducing thrust decreases the sound power radiated; decreasing climb airspeed permits the initiation of climb sooner and hence results in increasing the source to observer distance. In general, minimum sound-pressure levels are obtained by using a combination of both minimum thrust and minimum climb speed consistent with satety consideration.
Book Details
- Public Domain: Yes
- Country: US
- Published: 1956
- Publisher: National Advisory Committee for Aeronautics
- Language: English
- Pages: 19
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