Results 111 to 120 of about 1,929,704 (249)

Forward acoustic performance of a shock-swallowing high-tip-speed fan (QF-13) [PDF]

open access: yes
Forward noise and overall aerodynamic performance data are presented for a high-tip-speed fan having rotor blade airfoils designed to alter the conventional leading-edge bow shocks to weak, oblique shocks which are swallowed within the interblade ...
Lucas, J. G.   +2 more
core   +1 more source

Jet noise suppression by porous plug nozzles [PDF]

open access: yes
Jet noise suppression data presented earlier by Maestrello for porous plug nozzles were supplemented by the testing of a family of nozzles having an equivalent throat diameter of 11.77 cm.
Bauer, A. B., Kibens, V., Wlezien, R. W.
core   +1 more source

Interim noise correlation for some OTW configurations using external jet-flow deflectors [PDF]

open access: yes
Jet flap interaction acoustic data obtained statically from a model-scale study of STOL-OTW configurations with a conical nozzle mounted above the wing and using various external deflectors to provide jet-flow attachment are correlated. The acoustic data
Groesbeck, D. E., Vonglahn, U. H.
core   +1 more source

Aerodynamic and acoustic performance of ejectors for engine-under-the-wing concepts [PDF]

open access: yes
Subsonic thrust augmentation, exhaust plume velocity contours and acoustic characteristics of a small-scale, 6-tube mixer nozzle with ejector were obtained with and without a wing. Thrust augmentation up to 30 percent was achieved.
Goodykoontz, J. H.   +2 more
core   +1 more source

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