An experimental study of the effects of upstream obstructions upon subsonic jet noise

1974 ◽  
Vol 37 (2) ◽  
pp. 205-234 ◽  
Author(s):  
K.K. Ahuja
2005 ◽  
Vol 333 (10) ◽  
pp. 746-753 ◽  
Author(s):  
Vincent Fleury ◽  
Christophe Bailly ◽  
Daniel Juvé

1957 ◽  
Vol 61 (554) ◽  
pp. 112-114
Author(s):  
K. W. Hetzel

Reports of noise effects on the rear fuselage structure of large British aircraft indicated that one might expect noise damage in this region on the Vickers Supermarine Type 544 aircraft. It will be seen from Fig. 1 that the jet efflux from each engine passes close to the fuselage side and under the tailplane. The fuselage structure proper is, however, protected from the heat and noise effects at the jet efflux by a fairing which is insulated at all attachments. This fairing, by virtue of its shape, is called the “ pen nib. ”


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