Relevant bibliographies by topics / Propeller 1045

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  2. Dissertations / Theses
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  4. Conference papers

Academic literature on the topic 'Propeller 1045'

Author: Grafiati
Published: 7 June 2025
Last updated: 2 August 2025

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Journal articles on the topic "Propeller 1045"

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Markovska, Lubov, Oleksii Makovii, and Kateryna Balalaieva. "VERIFICATION OF THE TURBULENCE MODEL IN THE SIMULATION OF THE FLOW AROUND THE PROPELLER OF A BIPLANE." Annali d'Italia 64 (February 27, 2025): 64–74. https://doi.org/10.5281/zenodo.14937530.

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The paper presents the results of a physical and numerical experiment to measure the thrust generated by a UAV propeller. The analysis of the results shows that the discrepancy between the results of the physical and numerical experiments ranges from 1 to 12%
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Yamish Singh, Rajanarasimha Sangam, and Abhijeet Karmarkar. "Assembly and Programming of Hexacopter Drone for Surveillance and Medical Kit Delivery Purposes." International Research Journal on Advanced Engineering Hub (IRJAEH) 2, no. 06 (2024): 1794–803. http://dx.doi.org/10.47392/irjaeh.2024.0246.

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The project aims to assemble and program a hexacopter drone that can serve the purpose of surveillance in terrains and the delivery of medical kits in remote locations autonomously. Delivery of medical kits using drone technology resolves traffic issues faced by the ambulance during medical emergencies on the other hand drone technology also helps with surveillance in aerial monitoring, military, and agriculture. This Hexacopter drone is assembled by motors, 1045 propellers, Pixhawk flight controller, Electronic Speed Controller [ESC], S550 Frame, GPS module, 12 channel receiver, and transmitt
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Saputra, Dwiki Agung, and Jojo Sumarjo. "Perencanaan Ulang Propeller Shaft pada Mobil Toyota Kijang Super 1500cc Tahun 1990." Volume 23, Issue 2 32, no. 2 (2021): 115–21. http://dx.doi.org/10.23969/infomatek.v23i2.4376.

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Mobil merupakan salah satu jenis kendaraan pribadi yang biasa digunakan dalam kehidupan sehari-hari. Kendaraan dapat berjalan/bergerak karena ada sistem yang memindahkan tenaga/momen/putaran dari mesin ke roda. Jenis dan merk tersebut juga banyak, salah satunya yaitu Kijang Super 1500cc dari Toyota. Mobil jenis ini memiliki komponen penting di antaranya body (bodi), machine (mesin), suspension (suspensi), electrical (kelistrikan), wheel (roda), chasis (rangka). Rangka merupakan salah suatu bagian penting dalam kendaraan. Komponen rangka sendiri terdiri dari flange yoke, propeller shaft, univer
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Indreswari, Suroso, and Irmawan Erwhin. "Analysis of UAV multicopter of air photography in New Yogyakarta International Airports." TELKOMNIKA Telecommunication, Computing, Electronics and Control 17, no. 1 (2019): 521–28. https://doi.org/10.12928/TELKOMNIKA.v17i1.9255.

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The higher the quality of the drone, the longer the drone will fly and the better the quality of the drone's photography. Survey of research location in Glagah Indah Beach, preparation of drone at ground, we plan the height of flying drones, then testing drone at ground, we measure camera calibration, and then result capture in the air and images in the air. Vehicle specifications are as follows: Frame: F450; Flight Controller: DJI Naza M-Lite; Propeller: 1045 Prop; motorbike: brushless sunnsky 980 kVa; ESC: Skywalker 40 Ampere 3s; Battery: Ace 3s Gens 5000 mAH; Remote: Turnigy 9XR with Fr
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Tumur-Ochir, Erdenebat, Erdenebat Batzorigt, and Ganbat Danaa. "An Analysis of Increasing Thrust of an Air Propeller Through Additional Lift Surface." Proceedings of Higher Educational Institutions. Маchine Building, no. 12 (717) (December 2019): 87–93. http://dx.doi.org/10.18698/0536-1044-2019-12-87-93.

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Air propellers used in small scale unmanned aircraft operate at low Reynolds numbers. The aerody-namic force occurring on the blade when the air propeller is in operation is of variable nature. It is observed that for Reynold numbers below 5⋅105 flow separation can occur on some sections of the propeller surface. To deal with the problem, increase the lift on the blade and therefore, reduce the turbulence boundary level, a new design called bi-blade propeller is developed and patented. This design features an additional blade above the main one. Using ANSYS Fluent, samples of the bi-blade prop
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Suroso, Indreswari. "Analysis Of Mapping Multicopter Drones In The Entrance Area Of Prospective New Airports In Congot, Temon, Kulonprogo, Yogyakarta." Journal of Applied Geospatial Information 2, no. 2 (2019): 130–34. http://dx.doi.org/10.30871/jagi.v2i2.952.

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This research use multicopter drone. This mapping was carried out at the entrance area of the prospective new airport precisely at the Congot beach area, Temon district, Kulonprogo district with a multicopter drone. This drone is capable of recording an altitude of 100 meters above ground level and can photograph an area of 1.5 km. This study used a drone type multicopter The vehicle specifications are as follows: Frame: F450; Flight Controller: DJI Naza M-Lite; Propeller: 1045 Prop; motorbike: brushless sunnsky 980 kVa; ESC: Skywalker 40 Ampere 3s; Battery: Ace 3s Gens 5000mAH; Remote: Turnig
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Suroso, Indreswari. "Analisis Foto Udara dengan Multicopter di Daerah Penghasil Pasir Besi Karangwuni, Temon, Kulon Progo." Rekam 16, no. 1 (2020): 29–35. http://dx.doi.org/10.24821/rekam.v16i1.3474.

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Aerial Photo Analysis Using Multicopters in the Iron-Sand Producing Area in Karangwuni, Temon, Kulon Progo. This research was conducted in areas that have the potential for iron-sand, which is in Karangwuni village, Temon Subdistrict, Kulon Progo regency. The aim of this research is to examine the surface of the largest iron-sand producing areas in Kulon Progo. The specifications of the drones used in this research are as follows: frame :F450Flight Control: DJI Naza M-Lite; Propeller: 1045 Prop; Motorcycle: brushless sunnsky 980 kVa; ESC: Skywalker 40 Ampere 3s; Battery: Ace 3s Gens 5000mAH; R
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Li, Yong Xian, Wen Qiong Zhang, and Song Ping Chen. "Reliability Optimization Design of Automobile Propeller Shaft." Advanced Materials Research 1049-1050 (October 2014): 842–45. http://dx.doi.org/10.4028/www.scientific.net/amr.1049-1050.842.

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Large sag due to heavy weight of the propeller shaft is a major cause of rotating vibration, so that to use the hollow shaft is an effective way to reduce the weight. Many scholars and engineers ignored that the outer and inner diameter are discrete and integer variables in optimization design of the propeller shaft. The practicability of an optimal solution is affected by decimal value of the diameter. A practical reliability optimization model with discrete and integer variable of the propeller shaft is proposed, and “Solver” in Microsoft Excel is used to seek the solution of optimization de
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Neskoromnyy, Е. V., and D. S. Markov. "Methodology for Determining the Survivability and Resistance of Aircraft Propellers to the Impact of Foreign Objects." Proceedings of Higher Educational Institutions. Маchine Building, no. 10 (715) (October 2019): 93–102. http://dx.doi.org/10.18698/0536-1044-2019-10-93-102.

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The authors propose a technique for determining the survivability and resistance of the blades to impact by foreign objects located on the surface of the airfield pavement, using a set of mathematical models and experimental plants and considering the data on the layout and design of the aircraft and its propulsion system with a propeller. An example of the technique’s application to a small-sized aircraft with a propulsion system with a pushing propeller is considered. The results of theoretical studies on determining the boundaries and parameters of the impact of foreign objects with the pro
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Chandraker, Akhilesh, VM Victor, RK Naik, and AK Dave. "Battery powered self-propelled sowing machines: A review." International Journal of Advanced Biochemistry Research 8, no. 4S (2024): 521–24. http://dx.doi.org/10.33545/26174693.2024.v8.i4sg.1045.

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Dissertations / Theses on the topic "Propeller 1045"

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Peterson, Derek T. "Surface piercing propeller performance." Thesis, Monterey, California. Naval Postgraduate School, 2005. http://hdl.handle.net/10945/2046.

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This thesis addresses possible improvements in the efficiency (thrust) of surface piercing propellers; in particular with respect to the angle of the propeller shaft came to mind. Preliminary calculations based on the basic pitch/diameter geometry suggest that about 3-5% efficiency is lost if the shaft is parallel to the flow, compared to skewed a few degrees in the "paddlewheel" direction at certain speeds. More accurate calculations based on the lift characteristics of each blade, on the angle of attack and the flow of water over each blade and given a set of basic assumption on the over all
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Dane, Carl W. "Exploratory experimental investigation of a wave propeller." Thesis, Monterey, California. Naval Postgraduate School, 1992. http://hdl.handle.net/10945/23671.

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Flood, Kevin M. "Propeller performance analysis using lifting line theory." Thesis, Cambridge Massachusetts Institute of Technology, 2009. http://hdl.handle.net/10945/4308.

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CIVINS<br>Approved for public release, distribution unlimited<br>Propellers are typically optimized to provide the maximum thrust for the minimum torque at a specific number of revolutions per minute (RPM) at a particular ship speed. This process allows ships to efficiently travel at their design speed. However, it is useful to know how the propeller performs during off-design conditions. This is especially true for naval warships whose missions require them to perform at a wide range of speeds. Currently the Open-source Propeller Design and Analysis Program can design and analyze a propeller
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Kim, Gary G. "Numerical analysis of ice impacts on azimuth propeller." Thesis, Monterey, California: Naval Postgraduate School, 2013. http://hdl.handle.net/10945/37649.

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Approved for public release; distribution is unlimited<br>Incorporating an azimuth/podded propulsion into an ice-capable ship brings concern in the propellers durability and lifecycle. An ice impact model was constructed to have a better understanding of collisions occurring between ice and azimuth/podded propeller for ice operation ships. A typical propeller profile was created using MATLAB and modeled in SolidWorks using realistic material properties. The ANSYS Explicit Dynamics solver was used to simulate the ice-propeller impact. By conducting a parametric study, the ice impact model displ
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Neiusma, William J. Jr. "An investigation of two-propeller tilt wing V/STOL aircraft flight characteristics." Thesis, Monterey, California. Naval Postgraduate School, 1993. http://hdl.handle.net/10945/39820.

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Approved for public release, distribution is unlimited<br>The results of a two-propeller tilt wing aircraft static stability and performance simulation utilizing a NASA-Ames computer code, Tilt Wing Application General (TWANG), are presented with comparisons to actual test flight data. The Canadair CL-84 tilt wing aircraft was used as a model for the geometric data utilized by the computer simulation. Aerodynamic data for the simulation were obtained from previous NASA Ames research related to a four-propeller model. Variables used included a wide range of parameters associated with flig
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Koptu, Tolga. "Protecting the Turkish Straits from Maritime Terrorism: a Scheme to Impede Propeller Efficiency." Thesis, Monterey, California. Naval Postgraduate School, 2012. http://hdl.handle.net/10945/7370.

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The protection of the Turkish Straits against maritime terrorism is an important security problem that must be solved because the straits are highly vulnerable to terrorist attacks. The main purpose of this research is to increase the security of the Turkish Straits against maritime terrorism by designing an underwater system that can stop a terrorist ship by impeding its propeller efficiency. The underwater system wraps ropes and nets around the propeller and its hub, decreasing the propeller efficiency. First, the most probable scenario from the point of view of a terrorist organization is d
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Jinkerson, Richard Alan. "Constrained and unconstrained localization for automated inspection of marine propellers." Thesis, Monterey, California. Naval Postgraduate School, 1991. http://hdl.handle.net/10945/25782.

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England, Carolyn J. "Analysis of microstructure refinement during single-pass and multi-pass friction stir processing of NiAl propeller bronze." Thesis, Monterey, California. Naval Postgraduate School, 2010. http://hdl.handle.net/10945/5167.

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Approved for public release; distribution is unlimited<br>High strength, corrosion resistance, ductility, and toughness are material properties required for United States Navy (USN) Propellers. Propellers for both surface ships and submarines in the USN are currently made from cast Nickel Aluminum Bronze (NAB) Wrought NAB exhibits strength, corrosion resistance, high dampening capacity, low friction coefficients, and good fracture toughness for a wide range of temperatures [1]. Casting NAB into large structures lowers some of the qualities seen in wrought material and sought after for the
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Watkins, Lance J. "Self-propelled semi-submersibles the next great threat to regional security and stability." Thesis, Monterey, California. Naval Postgraduate School, 2011. http://hdl.handle.net/10945/5629.

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Approved for public release; distribution is unlimited.<br>The most effective and fastest-evolving delivery system for cocaine to move from its place of production in Colombia to the United States market has undoubtedly become the Self-Propelled Semi-Submersible (SPSS). Often called "drug subs" or "narco submarines," SPSSs are used to transport cocaine from Colombia's Pacific coast into Central America and Mexico, then overland to the United States. This thesis begins with an examination of the evolution of the illegal narcotics trade in Colombia since the 1990s. It examines the actions of Uni
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Beckett, David R. "An Integrated Hydrofoil and Propeller Design Tool for the Windows Environment." Thesis, 1996. http://hdl.handle.net/10945/24306.

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CIVINS<br>An investigation of the feasibility and desirability of the employment of personal computers in hydrofoil and propeller design was performed. The feasibility and desirability of the employment of personal computers in hydrofoil and propeller design was demonstrated by the seamless linking of the MIT Propulsor Lifting Line Code and the MIT Propeller Blade Design Code into a single Microsoft Windows(TM) based application.
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Books on the topic "Propeller 1045"

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The Self-Propelled Industrial Trucks (EEC Requirements) (Amendment) Regulations 1989 (Statutory Instruments: 1989: 1035). Stationery Office Books, 1989.

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Conference papers on the topic "Propeller 1045"

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Bowles, Patrick, Ben Berry, Emily Bartz, Claude Matalanis, Brian Wake, and Mark Scott. "A Model-Scale Wind-Tunnel Study of Main Rotor/Propeller Interference." In Vertical Flight Society 72nd Annual Forum & Technology Display. The Vertical Flight Society, 2016. http://dx.doi.org/10.4050/f-0072-2016-11591.

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A model-scale wind tunnel test was conducted to determine propulsive efficiency and relative vibration levels of a tail mounted propeller in the wake of a powered rotor and generic fuselage. Six-component propeller loads were measured for all test points with a focus on thrust and torque. Propeller and main rotor operating conditions were set to mimic low- and highspeed vehicle flight operations, simulating speeds from 105 kts to 200 kts. A total pressure wake survey conducted without the propeller installed was used to determine the propeller plane inflow characteristics. Propeller operation
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Jusko, Tim, and Tom Berger. "Piloted Simulation Evaluation of MTEs for the Assessment of Low-Level Handling Qualities." In Vertical Flight Society 80th Annual Forum & Technology Display. The Vertical Flight Society, 2024. http://dx.doi.org/10.4050/f-0080-2024-1048.

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This study introduces three new proposed Mission Task Elements (MTEs) - "Big Air", "Giant Slalom", and "Super Combined" - aimed at evaluating handling qualities during low-level and high-speed flight profiles. These MTEs are designed to reflect operational task elements critical in military engagements, particularly where rotorcraft capabilities in evading radar detection and maneuvering at high speeds are paramount. Utilizing piloted simulations with four generic rotorcraft configurations under various flight control laws, the MTEs' effectiveness in exposing aircraft characteristics and handl
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Trembois, Nikos, Michael Marques Goncalves, Austin D. Thai, and Jeremy J. Bain. "Assessment of Self-Noise Models Using NFAC Measurements of the Joby Aviation Propeller." In AIAA SCITECH 2025 Forum. American Institute of Aeronautics and Astronautics, 2025. https://doi.org/10.2514/6.2025-1045.

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Schroijen, Marcel, and Ronald Slingerland. "Propeller Slipstream Effects on Directional Aircraft Control with One Engine Inoperative." In 45th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2007. http://dx.doi.org/10.2514/6.2007-1046.

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ELLIOTT, S., P. NELSON, I. STOTHERS, C. BOUCHER, and J. EVERS. "In-flight experiments on the active control of propeller-induced cabin noise." In 12th Aeroacoustic Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-1047.

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Wickersheim, Robin, Jatinder Goyal, Tomas Sinnige, and Manuel Keßler. "Computational Cross-Validation of Propeller Noise in Positive and Negative Thrust Conditions." In AIAA SCITECH 2025 Forum. American Institute of Aeronautics and Astronautics, 2025. https://doi.org/10.2514/6.2025-1046.

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Fei, Xiaofan. "Evaluation of a Commercial Surface Vorticity Flow Solver for the Modeling of Propeller-Wing Interaction." In AIAA Scitech 2019 Forum. American Institute of Aeronautics and Astronautics, 2019. http://dx.doi.org/10.2514/6.2019-1046.

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McDonald, Robert A. "Modeling of Electric Motor Driven Variable Pitch Propellers for Conceptual Aircraft Design." In 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-1025.

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Leme, Felipe, and Thiago Pontin Tancredi. "IMPACT OF THE CHORD/DIAMETER DISTRIBUTION ON PROPELLERS EFFICIENCY USING THE LIFTING-LINE THEORY." In 26th International Congress of Mechanical Engineering. ABCM, 2021. http://dx.doi.org/10.26678/abcm.cobem2021.cob2021-1065.

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Xu, B., J. Li, and Z. Liu. "MODELING THE FORMATION AND PENETRATION OF A HIGH-SPEED JETTING PROJECTILE CHARGE." In 34th International Symposium on Ballistics. Destech Publications, Inc., 2025. https://doi.org/10.12783/ballistics25/37253.

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In this study, experiments and numerical analyses have been carried out to investigate the performance of a modified high-speed Jetting Projectile Charge (JPC) based on a Explosively Formed Projectile (EFP). A medium-carbon steel (AISI 1045) target was used in the penetration experiments of the modified JPC and the conventional EFP. The tip velocity of the metal jet before penetration was measured using speed sensors. The length to diameter ratio of The EFP is 1:1, the shell thickness is 5 mm, and the linear thickness is 1.8mm. The formation and penetration performance of the modified shaped c
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