Results 101 to 110 of about 1,052,955 (228)
Change of Pitch in certain Sounds with Distance [PDF]
, 1901 FREDERICK M. WEST
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Observation of a Further Tartini Pitch Resulting from a Physical Sinusoid Added to a Tartini Pitch [PDF]
, 1953 Max F. Meyer
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Acoustic and aerodynamic testing of a scale model variable pitch fan [PDF]
A fully reversible pitch scale model fan with variable pitch rotor blades was tested to determine its aerodynamic and acoustic characteristics. The single-stage fan has a design tip speed of 1160 ft/sec (353.568 m/sec) at a bypass pressure ratio of 1.5 ...
Jutras, R. R., Kazin, S. B.
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On the Damping Force and added Mass of Ships Heaving and Pitching
, 1959 Fukuzo Tasai
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Effects of dynamic aeroelasticity on handling qualities and pilot rating [PDF]
Pilot performance parameters, such as pilot ratings, tracking errors, and pilot comments were determined for a longitudinal pitch tracking task using a large, flexible bomber with parametric variations in the undamped natural frequencies of the two ...
Swaim, R. L., Yen, W. Y.
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PRODUCTION OF CARBON FIBERS FROM CASTILLA'S CRUDE-OIL DEASPHALTED BOTTOMS
CT&F Ciencia, Tecnología & Futuro, 2002 Obtaining raw materials for the manufacturing of carbon fibers from Castilla's crude-oil deasphalted bottoms was achieved through thermal treatments carried out in inert atmosphere, at temperatures ranging from 573 K to 673 K.
Gonzalo Leal, Jhon-Iván Peñaloza
doaj
Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability [PDF]
A static investigation of the internal performance of two short take-off and landing (STOL) nozzle concepts with pitch thrust-vectoring capability has been conducted.
Burley, J. R., II, Mason, M. L.
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USAGE OF COMPUTERISED MEANS IN VOCAL ASSESSMENT
Studia Universitatis Babeş-Bolyai. Musica, 2012 This study investigates implementation of new technologies in vocal assessment pertaining to university degree artistic education. One of our objectives represents the collection of information regarding changes occurring in singing voice as a result of
Ana RUSU
doaj
Dynamics of high-bypass-engine thrust reversal using a variable-pitch fan [PDF]
The test program demonstrated that successful and rapid forward-to reverse-thrust transients can be performed without any significant engine operational limitations for fan blade pitch changes through either feather pitch or flat pitch.
Sagerser, D. R. +2 more
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