Academic literature on the topic 'Compressed air propulsion'

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Compressed air propulsion.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Compressed air propulsion"

1

A. H. E., Gherouat, Khochemane L., and BENNIS O. "Marine Propulsion by the Injection of Compressed Air." International Journal of Engineering and Technology 8, no. 6 (2016): 3082–92. http://dx.doi.org/10.21817/ijet/2016/v8i6/160806406.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Wyczalek, Floyd A., та Chung M. Suh. "AirСar CAES-Compressed Air Energy Source-Compendium". Advanced Materials Research 430-432 (січень 2012): 189–96. http://dx.doi.org/10.4028/www.scientific.net/amr.430-432.189.

Full text
Abstract:
This paper is a re evaluation of CAES Compressed Air Energy Source. CAES is not new, experimental air car compressed air propulsion vehicles appeared in early 1900’s, and are currently exemplified by the India Tata Motors AirCar MiniCat based on the French MDI Motor Development International AirCar. (see Ulf Bossel, European Fuel Cell Forum) This study focuses on compressed air potential pressure specific energy density and specific power, ideal Global thermodynamic cycle efficiency, US EPA 23 cycle urban driving test schedule overall drive train ideal efficiency and vehicle ideal range. CAES
APA, Harvard, Vancouver, ISO, and other styles
3

Gasparini Croce, Rodrigo, Antônio Dariva, Emerson Pereira Trarbach, and Filipe Arthur Firmino Monhol. "Avaliação da eficiência na geração de energia elétrica de um motor híbrido (combustão + ar comprimido) a partir de testes em protótipo real." Latin American Journal of Energy Research 7, no. 1 (2020): 34–45. http://dx.doi.org/10.21712/lajer.2020.v7.n1.p34-45.

Full text
Abstract:
The continuous research for high efficiency and low emission engines are the technological challenges nowadays. Internal combustion engines are widely used due to low-cost if compared to the electrical vehicles' propulsion systems. Unfortunately, internal combustion engines have low efficiency; about 20%-25% are converted to mechanical power. A new hybrid approach engine running on ethanol and compressed air is presented in this paper. As a result, the global engine efficiency is improved once a part of energy comes from compressed air stored in an external reservoir. By measuring the ethanol
APA, Harvard, Vancouver, ISO, and other styles
4

UCHIMIYA, Takurou, and Masahiko SAKAMOTO. "G305 Ship Propulsion Equipment Directly Driven by Air Compressed by Self-Exited Vibration in Blower Piping System." Proceedings of the Fluids engineering conference 2012 (2012): 485–86. http://dx.doi.org/10.1299/jsmefed.2012.485.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Balan, George Iulian, Octavian Narcis Volintiru, Ionut Cristian Scurtu, Florin Ioniță, Mirela Letitia Vasile, and Claudia Borzea. "Considerations regarding the anti-icing system for the ship propulsion plant with gas turbine." E3S Web of Conferences 286 (2021): 04013. http://dx.doi.org/10.1051/e3sconf/202128604013.

Full text
Abstract:
Vessels that have navigation routes in areas with ambient temperatures that can drop below + 5 [°C], with a relative humidity of over 65%, will have implemented technical solutions for monitoring and combating ice accumulations in the intake routes of gas turbine power plants. Because gas turbines are not designed and built to allow the admission of foreign objects (in this case - ice), it is necessary to avoid the accumulation of ice through anti-icing systems and not to melt ice through defrost systems. Naval anti-icing systems may have as a source of energy flow compressed air, supersaturat
APA, Harvard, Vancouver, ISO, and other styles
6

SAKAMOTO, Masahiko, and Takurou Uchimiya. "121 A Ship Propulsion Equipment Driven by Air Compressed by Pressure Fluctuation in a Blower Piping System : Effect of Valve in Pipe." Proceedings of Conference of Kansai Branch 2013.88 (2013): _1–21_. http://dx.doi.org/10.1299/jsmekansai.2013.88._1-21_.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

UCHIMIYA, Takurou, and Masahiko SAKAMOTO. "G1001 Ship Propulsion Equipment Driven by Air Compressed by Self-Exited Vibration in Blower Piping System (Effect on Valve in Piping System)." Proceedings of the Fluids engineering conference 2013 (2013): _G1001–01_—_G1001–02_. http://dx.doi.org/10.1299/jsmefed.2013._g1001-01_.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Korakianitis, T., L. Meyer, M. Boruta, and H. E. McCormick. "One-Disk Nutating-Engine Performance for Unmanned Aerial Vehicles." Journal of Engineering for Gas Turbines and Power 126, no. 3 (2004): 475–81. http://dx.doi.org/10.1115/1.1496770.

Full text
Abstract:
The nutating engine is a new type of internal combustion engine. The engine has unique advantages over conventional piston engines and gas turbines in small power ranges suitable for unmanned aerial vehicles (UAV), and other applications. This publication is the original presentation of the performance potential of the simplest version of the engine, a one-disk engine operating at constant compression ratio, for light airframe propulsion. In its basic configuration the core of the engine is a nutating nonrotating disk, with the center of its hub mounted in the middle of a Z-shaped shaft. The t
APA, Harvard, Vancouver, ISO, and other styles
9

Tafti, Danesh K., Long He, and K. Nagendra. "Large eddy simulation for predicting turbulent heat transfer in gas turbines." Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences 372, no. 2022 (2014): 20130322. http://dx.doi.org/10.1098/rsta.2013.0322.

Full text
Abstract:
Blade cooling technology will play a critical role in the next generation of propulsion and power generation gas turbines. Accurate prediction of blade metal temperature can avoid the use of excessive compressed bypass air and allow higher turbine inlet temperature, increasing fuel efficiency and decreasing emissions. Large eddy simulation (LES) has been established to predict heat transfer coefficients with good accuracy under various non-canonical flows, but is still limited to relatively simple geometries and low Reynolds numbers. It is envisioned that the projected increase in computationa
APA, Harvard, Vancouver, ISO, and other styles
10

Gavrilescu, Ileana. "Effective business models for electric vehicles." Proceedings of the International Conference on Business Excellence 11, no. 1 (2017): 36–44. http://dx.doi.org/10.1515/picbe-2017-0004.

Full text
Abstract:
Abstract The proposed study aims to use asyncretic and synthetic approach of two elements that have an intrinsic efficiency value: business models and electric vehicles. Our approach seeks to circumscribe more widespread concerns globally - on the one hand, to oil shortages and climate change - and on the other hand, economic efficiency to business models customized to new types of mobility. New “electric” cars projects besiege the traditional position of the conventional car. In the current economy context the concept of efficiency of business models is quite different from what it meant in a
APA, Harvard, Vancouver, ISO, and other styles
More sources

Dissertations / Theses on the topic "Compressed air propulsion"

1

Silva, Junior Gilberto Caetano da [UNESP]. "Método dos mínimos quadrados aplicados ao lançamento de foguetes propulsionados a ar comprimido." Universidade Estadual Paulista (UNESP), 2017. http://hdl.handle.net/11449/152165.

Full text
Abstract:
Submitted by GILBERTO CAETANO DA SILVA JÚNIOR null (gilcaju@ig.com.br) on 2017-11-12T23:01:48Z No. of bitstreams: 1 versão definitiva.pdf: 1724008 bytes, checksum: c953406384f7a6ee2d78df6e9f2ae70b (MD5)<br>Submitted by GILBERTO CAETANO DA SILVA JÚNIOR null (gilcaju@ig.com.br) on 2017-11-22T14:06:59Z No. of bitstreams: 1 versão definitiva.pdf: 1724008 bytes, checksum: c953406384f7a6ee2d78df6e9f2ae70b (MD5)<br>Submitted by GILBERTO CAETANO DA SILVA JÚNIOR null (gilcaju@ig.com.br) on 2017-11-22T18:09:14Z No. of bitstreams: 1 versão definitiva.pdf: 1724008 bytes, checksum: c953406384f7a6ee2d
APA, Harvard, Vancouver, ISO, and other styles

Book chapters on the topic "Compressed air propulsion"

1

Kollmann, Karl, Calum E. Douglas, and S. Can Gülen. "Alternative Systems." In Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students. ASME, 2021. http://dx.doi.org/10.1115/1.884676_ch8.

Full text
Abstract:
The idea of precompression of the cylinder charge air is as old as the internal combustion itself. It is generally accepted that the first supercharger design in the modern sense was actually a turbocharger, patented in 1905 by the Swiss engineer Alfred Büchi (1879-1959). It comprised an axial compressor, an aftercooler and an exhaust gas turbine applied to a radial piston-cylinder engine as shown in the German patent drawings in Figure 8-1. Not surprisingly, it took him more than two decades to make the system work due to low component efficiencies, i.e., the problem that bedeviled all early gas turbine inventors due to the insufficient knowledge of aerodynamics.
APA, Harvard, Vancouver, ISO, and other styles
2

Kollmann, Karl, Calum E. Douglas, and S. Can Gülen. "Exhaust Gas Turbine." In Turbo/Supercharger Compressors and Turbines for Aircraft Propulsion in WWII: Theory, History and Practice—Guidance from the Past for Modern Engineers and Students. ASME, 2021. http://dx.doi.org/10.1115/1.884676_ch10.

Full text
Abstract:
As discussed in Chapter 2, the supercharger (basically, an air compressor) can also be driven by an exhaust gas turbine. In this case, the overall system is referred to as a turbocharger or turbosupercharger (Abgasturbolader in German). The focus in Kollmann’s manuscript is exclusively on radial compressors used as superchargers driven by a gear drive connected to the main engine shaft. This is not so surprising considering that, although significant R&amp;D effort was spent on the turbine design (especially, turbine blade cooling), turbocharged German aircraft engines did not enter service until the end of the war. Even then, the service experience was limited to Junkers Ju 388 (mostly for high altitude reconnaissance) powered by two 1,500-HP BMW 801 J turbocharged engines. Many other designs (e.g., the DB 623) were eventually abandoned. The dilemma facing the German engineers at the time (1940s) was this: whether to develop an aircraft engine from the get-go with a turbocharger or to develop a turbocharger to be fitted into an existing engine (e.g., the DB 603). Since the need for the turbochargers arose during the war by the need for higher flight altitudes (10 to 14 km), e.g., to attack the Allied bomber formations and their fighter escort, the urgency of the situation made the choice for them1. Not surprisingly, they went with the latter option.
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Compressed air propulsion"

1

Alami, Abdul Hai, Noaf Alblooki, Muhammad Tawalbeh, Zainab Almerashi, Amna Alkharousi, and Tareq Salameh. "Compressed air for light vehicle propulsion." In 2020 Advances in Science and Engineering Technology International Conferences (ASET). IEEE, 2020. http://dx.doi.org/10.1109/aset48392.2020.9118278.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Carvalho, Leonardo de Oliveira. "Exergetic analysis of compressed air for vehicular propulsion." In 2008 SAE Brasil Congress and Exhibit. SAE International, 2008. http://dx.doi.org/10.4271/2008-36-0315.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Whitmore, Stephen A., and Anthony M. Bulcher. "A Green Hybrid Thruster Using Moderately Enriched Compressed Air as the Oxidizer." In 2018 Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 2018. http://dx.doi.org/10.2514/6.2018-4841.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Sakamoto, Masahiko. "Ship Propulsion Equipment Driven by Air Compressed by Pressure Fluctuation in Blower Piping System." In ASME 2013 Fluids Engineering Division Summer Meeting. American Society of Mechanical Engineers, 2013. http://dx.doi.org/10.1115/fedsm2013-16103.

Full text
Abstract:
The characteristics of thrust for ship propulsion equipment directly driven by air compressed by pressure fluctuation in a blower piping system are investigated. The pressure in the piping system with a discharge opening under the surface of water is measured for the depth and the cross-sectional area of the discharge opening. An exhaust valve is positioned upon the air ejection hole, and the effects of the valve on the pressure in the pipes and the thrust for the propulsive nozzle were examined. The following results were obtained. The pressure fluctuation owing to the columnar resonance or H
APA, Harvard, Vancouver, ISO, and other styles
5

Kirk, Daniel, Joel Faure, Hector Gutierrez, Stanislav Svetlov, Ronald Hayes, and Kevin Wang. "Generation and Analysis of Blast Waves from a Compressed Air-Driven Shock Tube." In 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-4777.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Asfar, Khaled, and Eyad Al-Smadi. "Water Piston Engine for Marine Vehicle Propulsion." In ASME-JSME-KSME 2019 8th Joint Fluids Engineering Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/ajkfluids2019-4824.

Full text
Abstract:
Abstract This paper describes an environment friendly propulsion system with negligible noise. The Propulsion system is based on a novel engine called a water piston engine. All moving parts in the classical internal combustion engine are eliminated; the piston, connecting rod, and crankshaft. Also, cams and follower valves are replaced by solenoid valves which inject compressed air into the cylinders. A water column in the cylinder is used to replace the metallic piston. The water column itself inside the cylinder acts as a piston. This Water Piston Engine is powered by pressurized air only.
APA, Harvard, Vancouver, ISO, and other styles
7

Murthy, M. S. N., Subhash Kumar, and Sheshadri Sreedhara. "Analysis of Part Electric Gas Turbine: A Novel Hybrid Propulsion Concept." In ASME 2019 Gas Turbine India Conference. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gtindia2019-2498.

Full text
Abstract:
Abstract A gas turbine engine (GT) is very complex to design and manufacture considering the power density it offers. Development of a GT is also iterative, expensive and involves a long lead time. The components of a GT, viz compressor, combustor and turbine are strongly dependent on each other for the overall performance characteristics of the GT. The range of compressor operation is dependent on the functional and safe limits of surging and choking. The turbine operating speeds are required to be matched with that of compressor for wide range of operating conditions. Due to this constrain,
APA, Harvard, Vancouver, ISO, and other styles
8

Korakianitis, T., L. Meyer, M. Boruta, and H. E. McCormick. "One-Disk Nutating-Engine Performance for Unmanned Aerial Vehicles." In ASME Turbo Expo 2001: Power for Land, Sea, and Air. American Society of Mechanical Engineers, 2001. http://dx.doi.org/10.1115/2001-gt-0466.

Full text
Abstract:
The nutating engine is a new type of internal combustion engine. The engine has unique advantages over conventional piston engines and gas turbines in small power ranges suitable for unmanned aerial vehicles (UAV), and other applications. This publication is the original presentation of the performance potential of the simplest version of the engine, a one-disk engine operating at constant compression ratio, for light airframe propulsion. In its basic configuration the core of the engine is a nutating non-rotating disk, with the center of its hub mounted in the middle of a Z-shaped shaft. The
APA, Harvard, Vancouver, ISO, and other styles
9

Kopasakis, George, Joseph W. Connolly, Daniel E. Paxson, and Peter Ma. "Volume Dynamics Propulsion System Modeling for Supersonics Vehicle Research." In ASME Turbo Expo 2008: Power for Land, Sea, and Air. ASMEDC, 2008. http://dx.doi.org/10.1115/gt2008-50524.

Full text
Abstract:
Under the NASA Fundamental Aeronautics Program the Supersonics Project is working to overcome the obstacles to supersonic commercial flight. The proposed vehicles are long slim body aircraft with pronounced aero-servo-elastic modes. These modes can potentially couple with propulsion system dynamics; leading to performance challenges such as aircraft ride quality and stability. Other disturbances upstream of the engine generated from atmospheric wind gusts, angle of attack, and yaw can have similar effects. In addition, for optimal propulsion system performance, normal inlet-engine operations a
APA, Harvard, Vancouver, ISO, and other styles
10

Woollatt, D. "A High Efficiency Valve for a Locomotive Air Brake Compressor." In Marine Propulsion Technology. SAE International, 1986. http://dx.doi.org/10.4271/860884.

Full text
APA, Harvard, Vancouver, ISO, and other styles
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!