Results
- Showing results for:
- Reset all filters
Search results
-
Book chapterChilds PRN, Masen MA, 2025,
Shafts
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 247-317, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Rolling element bearings
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 199-246, ISBN: 9780443220777 -
Book chapterHazeri K, Childs PRN, 2025,
Extension of the Consensual Assessment Technique to Consumer Products: Case Studies
, Creations, Publisher: Springer Nature Switzerland, Pages: 161-186, ISBN: 9783031824142 -
Book chapterChilds PRN, Masen MA, 2025,
Seals
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 595-658, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Bevel gears
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 419-454, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Design
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 1-59, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Engineering materials
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 61-80, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Tolerancing and precision engineering
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 803-849, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Worm gears
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 455-473, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Tribology
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 111-152, ISBN: 9780443220777 -
Book chapterThomopoulos N, Lin G, Jagannath S, et al., 2025,
Targeting Change for Active Travel
, Editors: Nathanail, Gavanas, Adamos, Publisher: SPRINGER INTERNATIONAL PUBLISHING AG, Pages: 154-180, ISBN: 978-3-031-82713-6 -
Journal articleLladó P, Majdak P, Barumerli R, et al., 2025,
Spectral Weighting of Monaural Cues for Auditory Localization in Sagittal Planes.
, Trends Hear, Vol: 29Localization of sound sources in sagittal planes significantly relies on monaural spectral cues. These cues are primarily derived from the direction-specific filtering of the pinnae. The contribution of specific frequency regions to the cue evaluation has not been fully clarified. To this end, we analyzed how different spectral weighting schemes contribute to the explanatory power of a sagittal-plane localization model in response to wideband, flat-spectrum stimuli. Each weighting scheme emphasized the contribution of spectral cues within well-defined frequency bands, enabling us to assess their impact on the predictions of individual patterns of localization responses. By means of Bayesian model selection, we compared five model variants representing various spectral weights. Our results indicate a preference for the weighting schemes emphasizing the contribution of frequencies above 8 kHz, suggesting that, in the auditory system, spectral cue evaluation is upweighted in that frequency region. While various potential explanations are discussed, we conclude that special attention should be put on this high-frequency region in spatial-audio applications aiming at the best localization performance.
-
Book chapterChilds PRN, Masen MA, 2025,
Journal bearings
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 153-198, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Pneumatics and hydraulics
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 779-801, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Spur and helical gear stressing
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 377-418, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Wire rope
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 763-778, ISBN: 9780443220777 -
Book chapterChilds PRN, Masen MA, 2025,
Gears
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 319-376, ISBN: 9780443220777 -
Conference paperSerafin S, Adjorlu A, Nordahl R, et al., 2025,
IEEE 8th VR Workshop on Sonic Interactions for Virtual Environments
, 2025 Conference on Virtual Reality and 3D User Interfaces Abstracts and Workshops-VRW, Publisher: IEEE COMPUTER SOC, Pages: 611-612 -
Conference paperBarumerli R, Privitera AG, Carollo A, et al., 2025,
Measuring Motor Planning Using an Affordable Sound -Based Virtual Reality Setup for Accessible Perception -Action Studies
, 2025 Conference on Virtual Reality and 3D User Interfaces Abstracts and Workshops-VRW, Publisher: IEEE COMPUTER SOC, Pages: 613-618 -
Conference paperZhang Z, Sun J, Peters D, et al., 2025,
Beyond Wellbeing Apps: Co-Designing Immersive, Embodied, and Collective Digital Wellbeing Interventions for Healthcare Professionals
, 2025 Designing Interactive Systems Conference-DIS, Publisher: ASSOC COMPUTING MACHINERY, Pages: 3132-3152 -
Conference paperCacciarelli D, Pinson P, Panagiotopoulos F, et al., 2025,
Causal Impact of Wind Energy on the UK Day-ahead Market
, 21st International Conference on the European Energy Market-EEM-Annual, Publisher: IEEE, ISSN: 2165-4077 -
Journal articleVamvakeros A, Papoutsellis E, Dong H, et al., 2025,
<i>nDTomo</i> : a modular Python toolkit for X-ray chemical imaging and tomography
, Digital Discovery, Vol: 4, Pages: 2579-2592<jats:p> <jats:italic>nDTomo</jats:italic> is a Python-based software suite for the simulation, reconstruction and analysis of X-ray chemical imaging and computed tomography data. </jats:p>
-
Conference paperde Vargas JMR, Schneider A, Pinson P, et al., 2025,
Data Sharing between Wind Energy Producers: Economic Incentives and Strategic Behavior
, 16th International Conference on Future and Sustainable Energy Systems-E-Energy, Publisher: ASSOC COMPUTING MACHINERY, Pages: 505-514 -
Conference paperShilov I, Le Cadre H, Busic A, et al., 2025,
Forecast Trading as a Means to Reach Social Optimum on a Peer-to-Peer Market
, 11th International Conference on Network Games, Control and Optimization, Publisher: SPRINGER INTERNATIONAL PUBLISHING AG, Pages: 121-130, ISSN: 0302-9743 -
Book chapterVohra S, Childs PRN, 2025,
Interplays Between Learning Theories
, Design Science and Innovation, Publisher: Springer Nature Singapore, Pages: 57-71, ISBN: 9789819773626 -
Journal articleWu J, Gao Z, Fu Z, et al., 2025,
Regulation of the cathode inner Helmholtz plane in dilute ether electrolytes using an electric-field-responsive solvent for high-voltage lithium metal batteries
, Energy & Environmental Science, ISSN: 1754-5692<jats:p>Herein, we demonstrate that the battery intrinsic electric field drives the specific adsorption of a weakly solvated co-solvent, DTS, to replace conventional DME in the IHP, enabling the desirable CEI chemistry on the 4.6 V LiCoO<jats:sub>2</jats:sub> cathode.</jats:p>
-
Book chapterChilds PRN, Masen MA, 2025,
Springs
, Mechanical Design Engineering Handbook, Publisher: Elsevier, Pages: 659-703, ISBN: 9780443220777 -
Journal articleJagtap SS, Childs PRN, Stettler MEJ, 2024,
Conceptual design-optimisation of a subsonic hydrogen-powered long-range blended-wing-body aircraft
, International Journal of Hydrogen Energy, Vol: 96, Pages: 639-651, ISSN: 0360-3199The adoption of liquid hydrogen (LH2) holds promise for decarbonising long-range aviation. LH2 aircraft could weigh less than Jet-A aircraft, thereby reducing the thrust requirement. However, the lower volumetric energy density of LH2 can adversely impact the aerodynamic performance and energy consumption of tube-wing aircraft. In a first, this work conducts an energy performance modelling of a futuristic (2030+) LH2 blended-wing-body (BWB) aircraft (301 passengers and 13,890 km) using conceptual aircraft design-optimisation approach employing weight-sizing methods, while considering the realistic gravimetric and volumetric energy density effects of LH2 on aircraft design, and the resulting reduction in aircraft thrust requirement. This study shows that at the design point the futuristic LH2 BWB aircraft reduces the specific energy consumption (SEC, MJ/tonne-km) by 51.7–53.5% and 7.3–10.8%, compared to (Jet-A) Boeing 777-200LR and Jet-A BWB, respectively. At the off-design points, this study shows that by increasing the load factor for a given range and/or increasing range for all load factor cases, the SEC (or energy efficiency) of this LH2 BWB concept improves. The results of this work will inform future studies on use-phase emissions and contrails modelling, LH2 aircraft operations for contrail reduction, estimation of operating costs, and lifecycle climate impacts.
-
Journal articleRiley S, Shevchuk A, George C, 2024,
Achieving dynamic stability and electromechanical resilience for ultra-flexible battery technology
, COMMUNICATIONS MATERIALS, Vol: 5 -
Journal articleJagtap SS, Childs PRN, Stettler MEJ, 2024,
Conceptual design-optimisation of a future hydrogen-powered ultrahigh bypass ratio geared turbofan engine
, International Journal of Hydrogen Energy, Vol: 95, Pages: 317-328, ISSN: 0360-3199Liquid hydrogen (LH2) is a proposed option to decarbonise long-haul aviation. LH2 aircraft (combustion-based) is expected to be lighter than Jet-A aircraft which necessitates reduction in the engine thrust requirement. Thus, the thermodynamic and energy performance of a LH2 aircraft engine, and its design and optimisation, is of significance. In a first, a conceptual design and optimisation of a future LH2 powered ultra-high bypass-ratio geared turbofan engine is conducted for reduced aircraft thrust requirement, using GasTurb 13 software and implementing future materials and component efficiencies. The thrust specific energy consumption (TSEC) of the optimised LH2 engine is 6–8% lower than Jet-A. The TSEC of LH2 engine is lower than Jet-A due to hydrogen's higher gravimetric energy density during combustion, higher specific heat of combustion products, and reduced thrust requirement. It is observed that optimised LH2 engine has 11% smaller diameter, 5.5–7.5% shorter length, 6–14% lower turbine entry temperature and 7.4–17.6% lower weight, than a Jet-A engine. The results of this work will be useful to future studies on LH2 engine and aircraft design, and LH2 aircraft emissions and contrails modelling.
This data is extracted from the Web of Science and reproduced under a licence from Thomson Reuters. You may not copy or re-distribute this data in whole or in part without the written consent of the Science business of Thomson Reuters.