Discussion: “Some Dynamic Properties of Oil-Film Journal Bearings With Reference to the Unbalance Vibration of Rotors” (Hagg, A. C., and Sankey, G. O., 1956, ASME J. Appl. Mech., 23, pp. 302–306) [PDF]
P. R. Trumpler
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Herein, a patient‐mounted neuro optical coherence tomography system that integrates a 5 degrees‐of‐freedom skull‐mounted robot (Skullbot) with a 0.6 mm neuroendoscope for targeted, minimally invasive deep brain imaging, is developed. The system offers high‐resolution imaging with precise deployment, demonstrated through successful tumor imaging in a ...
Chao Xu+7 more
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Closure to “Discussions of ‘Operating Experience With High-Temperature Steam-Turbine Rotors and Design Improvements in Rotor-Blade Fastening’” (1958, Trans. ASME, 80, pp. 1223–1224) [PDF]
J. D. Conrad, N. L. Mochel
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Morphy: A Compliant and Morphologically Aware Flying Robot
This study presents Morphy, a 25.2 cm‐wide, 260 g aerial robot with flexible, sensorized joints that enable it to withstand high‐speed collisions and squeeze through narrow spaces. Powered by an adaptive control scheme exploiting real‐time morphology feedback, Morphy demonstrates resilience in trajectory tracking, collision, and impact recovery and ...
Paolo De Petris+2 more
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Full Annular RUB in Mechanical Seals, Part I: Experimental Results
Donald E. Bently+3 more
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Discussion: “Acceptance Guides for Ultrasonic Inspection of Large Rotor Forgings” (Rankin, A. W., and Moriarty, C. D., 1956, Trans. ASME, 78, pp. 1603–1612) [PDF]
J. A. Succop
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Hover test of a full-scale hingeless rotor [PDF]
The performance and aeroelastic stability in hover of a 9.8-m diameter, hingeless helicopter rotor system was evaluated. Rotor performance and inplane damping data were obtained for rotor operation between 350 and 425 rpm for thrust coefficients (CT ...
Peterson, R. L., Warmbrodt, W.
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PairTilt: Design and Control of an Active Tilt‐Rotor Quadcopter for Improved Efficiency and Agility
PairTilt is an actuated tilt‐rotor unmanned aerial vehicle capable of active shape reconfiguration, balancing simplicity, efficiency, and agility. Its H‐shaped frame incorporates pairwise tiltable rotors, which reduce gyroscopic torque and decouple key dynamics, enhancing maneuverability and reducing drag.
Jerry Tang, Mark W. Mueller
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Closure to “Discussions of ‘Acceptance Guides for Ultrasonic Inspection of Large Rotor Forgings’” (1956, Trans. ASME, 78, pp. 1612–1619) [PDF]
A. W. Rankin, C. D. Moriarty
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Rotor performance characteristics from an aeroacoustic helicopter wind-tunnel test program [PDF]
An investigation of helicopter rotor noise at model scale was conducted in the Langley 4 by 7 meter tunnel. The program described was the first of a planned three-phase project whose purpose was to examine the characteristic noise mechanism involved in ...
Elliott, J. W., Hoad, D. R., Orie, N. M.
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