Design program of combination suppressor-reverser having internal clamshell type reverser mounted between suppressor and engine; prototype configuration consists of basic pressure vessel mounting 21 individual nozzles to meet attenuation requirements of JT-3 engine; nozzle attenuation characteristics; design of 9-tube unit with very nearly same attenuation characteristics as 21-tube nozzle.
Design, development and operational experience of Boeing 707 thrust reverser/sound suppressor
SAE -- Paper
SAE Meeting ; 1959 Thrust reversal
1959
10 pages
Conference paper
English
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DESIGN, DEVELOPMENT AND OPERATIONAL EXPERIENCE OF THE BOEING 707 THRUST REVERSER/SOUND SUPPRESSOR
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