Academic literature on the topic 'Turbo C++'

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Journal articles on the topic "Turbo C++"

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Challab, DJ. "Turbo C++." Information and Software Technology 34, no. 9 (1992): 617–18. http://dx.doi.org/10.1016/0950-5849(92)90140-k.

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Hughes, Larry. "Teaching operating systems using Turbo C." ACM SIGCSE Bulletin 24, no. 1 (1992): 181–86. http://dx.doi.org/10.1145/135250.134547.

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Park, K.-J., and D. Jung. "External condensation heat transfer coefficients of R22 alternative refrigerants on enhanced tubes at three saturation temperatures." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science 222, no. 6 (2008): 987–94. http://dx.doi.org/10.1243/09544062jmes933.

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In this study, external condensation heat transfer coefficients (HTCs) of R22, R410A, R407C, and R134a are measured on a 1024 fins per meter (26 fins per inch) low fin tube and Turbo-C tube at saturation temperatures of 30, 39, and 50 °C with wall subcooling of 3–8 °C. Test results show that condensation HTCs of all refrigerants decrease as the saturation temperature increases from 30 to 50 °C. This trend is due to the degradation of thermophysical properties of the liquid phase with an increase in saturation temperature. For the low fin tube data, Beatty and Katz's prediction equation showed
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Poljak, Igor, Ivica Glavan, Josip Orović, and Vedran Mrzljak. "Three Approaches to Low-Duty Turbo Compressor Efficiency Exploitation Evaluation." Applied Sciences 10, no. 10 (2020): 3373. http://dx.doi.org/10.3390/app10103373.

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This paper presents three approaches for isentropic, energy, and exergy evaluations of a low-duty liquid natural gas (LNG) vapor turbo compressor during exploitation on a conventional LNG carrier. The evaluation was conducted on the measured performance parameters under 22 various turbo compressor operating regimes. The turbo compressor performance was evaluated in the temperature span from −69 to −105 °C and during changes in the rpm of the main propulsion turbine and, consequently, the main boiler load. The results show that the highest measured turbo compressor isentropic efficiency is in a
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Lim, G. H. "Vibratory feeder motion study using Turbo C++ language." Advances in Engineering Software 18, no. 1 (1993): 53–59. http://dx.doi.org/10.1016/0965-9978(93)90007-g.

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Velásquez Rodríguez, Claudia María, and Juliana María Orozco Cano. "Dislipidemia en niños con desnutrición aguda. Turbo, Colombia." Perspectivas en Nutrición Humana 14, no. 2 (2013): 157–70. http://dx.doi.org/10.17533/udea.penh.16486.

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Objetivo: comparar el perfil lipídico de niños menores de 5 años con desnutrición aguda con ungrupo control. Metodología: estudio descriptivo, de corte transversal, en 43 niños, 26 con desnutriciónaguda y 17 con adecuado peso para la talla (P/T). Entre los grupos de estudio secompararon las concentraciones séricas de CT, c-LDL, c-HDL y TG. Resultados: el grupo condesnutrición presentó una frecuencia significativamente mayor de c-HDL bajas comparados concontroles (19 vs 7% respectivamente, p=0,036) y un riesgo 1,8 veces mayor de c-HDL bajas(OR=1,8; IC 0,960-3,280). Los TG fueron mayores en los
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Ferreira Lima, João Vicente, Issam Raïs, Laurent Lefèvre, and Thierry Gautier. "Performance and energy analysis of OpenMP runtime systems with dense linear algebra algorithms." International Journal of High Performance Computing Applications 33, no. 3 (2018): 431–43. http://dx.doi.org/10.1177/1094342018792079.

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In this article, we analyze performance and energy consumption of five OpenMP runtime systems over a non-uniform memory access (NUMA) platform. We also selected three CPU-level optimizations or techniques to evaluate their impact on the runtime systems: processors features Turbo Boost and C-States, and CPU Dynamic Voltage and Frequency Scaling through Linux CPUFreq governors. We present an experimental study to characterize OpenMP runtime systems on the three main kernels in dense linear algebra algorithms (Cholesky, LU, and QR) in terms of performance and energy consumption. Our experimental
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NAKAGAWA, Shin, Tomoya NAKAJIMA, Tomoaki ITANO, and Masako SUGIHARA-SEKI. "Measurements of Aerodynamic Characteristics of the Turbo-Jav." Proceedings of the Symposium on sports and human dynamics 2016 (2016): C—12. http://dx.doi.org/10.1299/jsmeshd.2016.c-12.

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Nugroho, S. D., C. Z. Pratiwi, and S. Holil. "The design of turbo jet surface aerator to enhance dissolved oxygen level in shrimp pond." IOP Conference Series: Earth and Environmental Science 1036, no. 1 (2022): 012102. http://dx.doi.org/10.1088/1755-1315/1036/1/012102.

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Abstract The dissolved oxygen (DO) is crucial water quality parameters for shrimp farming. The farmers need aerator to break water into fine drops or creating bubbles that can enhance dissolved oxygen level in the pond. Turbo jet surface aerator is the one type of aerator. This aerator works by rotating propeller which is connected by a hollow shaft to the motor. The angular adjustment that is used from the engine holder is 20°. Therefore, the propeller can rotate in half submerged position which is 4.5 cm immersion depth. This turbo jet surface aerator is designed using 0.5 HP electric motor,
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Setiyo, Muji, Sudjito Soeparman, Slamet Wahyudi, and Nurkholis Hamidi. "The Alternative Way to Drive the Automobile Air-Conditioning, Improve Performance, and Mitigate the High Temperature: A Literature Overview." Periodica Polytechnica Transportation Engineering 46, no. 1 (2017): 36. http://dx.doi.org/10.3311/pptr.8892.

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Over fuel consumption and increasing in CO2 emissions are problems as compensation from the imposition of automobile A/C systems. Another problem is the extreme temperature when the car is parked under sunlight so that the thermal load becomes very large when A/C is turned on. Therefore, this article presents various methods to overcome the problem. Methods to reduce fuel consumption and to reduce CO2 emissions are done by application of VCC and the absorption system. Potential of turbo A/C system and combining vapor compression and LPG fuel system has also been studied. Potential of turbo A/C
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Dissertations / Theses on the topic "Turbo C++"

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Turner, Edward Joseph. "Measurement Drift in 3-Hole Yaw Pressure Probes From 5 Micron Sand Fouling at 1050° C." Thesis, Virginia Tech, 2018. http://hdl.handle.net/10919/96811.

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3-hole pressure probes are capable of accurately measuring flow angles in the yaw plane. These probes can be utilized inside a jet engine hot section for diagnostics and flow characterization. Sand and other particulate pose a significant risk to hot section components and measurement devices in gas turbine engines. The objective of this experiment was to develop a better understanding of the sensitivity of experimental 3-hole pressure probe designs to engine realistic sand fouling. In this study, Wedge, Cylindrical, and Trapezoidal probes were exposed to realistic hot section turbine environ
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Gazi, Orhan. "Parallelized Architectures For Low Latency Turbo Structures." Phd thesis, METU, 2007. http://etd.lib.metu.edu.tr/upload/12608110/index.pdf.

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In this thesis, we present low latency general concatenated code structures suitable for parallel processing. We propose parallel decodable serially concatenated codes (PDSCCs) which is a general structure to construct many variants of serially concatenated codes. Using this most general structure we derive parallel decodable serially concatenated convolutional codes (PDSCCCs). Convolutional product codes which are instances of PDSCCCs are studied in detail. PDSCCCs have much less decoding latency and show almost the same performance compared to classical serially concatenated convolutional co
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Olsen, Donald P. "PROPOSED NEW WAVEFORM CONCEPT FOR BANDWIDTH AND POWER EFFICIENT TT&C." International Foundation for Telemetering, 1999. http://hdl.handle.net/10150/608730.

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International Telemetering Conference Proceedings / October 25-28, 1999 / Riviera Hotel and Convention Center, Las Vegas, Nevada<br>Most traditional approaches to TT&C have employed waveforms that are neither very power nor bandwidth efficient. A new approach to TT&C waveforms greatly improves these efficiencies. Binary Gaussian Minimum Shift Keying (GMSK) provides a constant envelope bandwidth efficient signal for applications above about 10 Kbps. The constant envelope preserves the spectrum through saturated amplifiers. It provides the best power efficiency when used with turbo coding. For p
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Abdullah, Nuruddin S. "The design of a PC software package to determine speed, skidding time, skidding distance and drag factor of vehicles implemented in turbo C for MS-DOS V 5.0." Ohio University / OhioLINK, 1994. http://rave.ohiolink.edu/etdc/view?acc_num=ohiou1176494304.

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Sousa, Aline Farias Gomes de. "Enumera??o de espectro de dist?ncias de esquemas de modula??o codificada em treli?a empregando codifica??o turbo." Universidade Federal do Rio Grande do Norte, 2010. http://repositorio.ufrn.br:8080/jspui/handle/123456789/15321.

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Made available in DSpace on 2014-12-17T14:55:43Z (GMT). No. of bitstreams: 1 AlineFGS_DISSERT.pdf: 1151209 bytes, checksum: 4ae192dd7519e3e14977154f7b70d951 (MD5) Previous issue date: 2010-06-14<br>Conselho Nacional de Desenvolvimento Cient?fico e Tecnol?gico<br>In this work, a performance analysis of transmission schemes employing turbo trellis coded modulation. In general, the performance analysis of such schemes is guided by evaluating the error probability of these schemes. The exact evaluation of this probability is very complex and inefficient from the computational point of view, a wi
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Becker, Celso Goncalves. "Otite média com efusão: estudo comparativo da eficácia da inserção do tubo de ventilação versus aplicação tópica de mitomicina C, após timpanotomia e aspiração da efusão." Universidade Federal de Minas Gerais, 2003. http://hdl.handle.net/1843/BUOS-9MPG9Q.

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A otite média com efusão constitui enfermidade de alta prevalência na população pediátrica. A disfunção da tuba auditiva é o principal fator etiológico por promover hipoventilação da orelha média, metaplasia do epitélio da cavidade timpânica e incremento de células caliciformes. A inserção de tubo de ventilação na membrana timpânica é o tratamento cirúrgico de eleição, substituindo temporariamente a função tubária, com grande eficácia na melhora auditiva e na prevenção de recorrências. No entanto, a inserção do tubo de ventilação não é isenta de complicações, além de promover prolongada limita
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Lee, Chia-Yu, and 李佳侑. "High Voltage Buck-Boost DC-DC Converter for Universal Serial Bus Type-C and Turbo Boost Technology." Thesis, 2016. http://ndltd.ncl.edu.tw/handle/hxkhmw.

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碩士<br>國立交通大學<br>電機工程學系<br>105<br>Recently, the latest Universal Serial Bus type-C connecter not only can transfer data but also deliver power. As mentioned in USB Power Delivery Specification Release 2.0 Version 1.2, USB type-C can deliver power ranged from 0.5W (100mA at 5V) to 100W (5A at 20V). In order to support such input range, the converter must be able to endure up 20V of input voltage. Also, the converter is required to support the latest Intel® turbo boost technology. Turbo boost technology, discussed in an Intel® November 2008 Whit paper, can enable the CPU to run above its base ope
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Books on the topic "Turbo C++"

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Perry, Greg M. Turbo C. Sams Publ, 1994.

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LeBlanc, Gérard. Turbo C. 4th ed. Eyrolles, 1989.

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International, Borland. Turbo C++. Borland International, 1990.

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Prokof'ev, B. P. Graficheskie sredstva Turbo c i Turbo C++. "Finansy I Statistika", Sp "Lanit", 1992.

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Schildt, Herbert. Using Turbo C. McGraw, 1987.

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Schildt, Herbert. Using Turbo C++. Osborne McGraw-Hill, 1990.

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Wang, Wally. Illustrated Turbo C++. Wordware Pub., 1991.

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Voss, Greg. Turbo C++ DiskTutor. 2nd ed. Osborne McGraw-Hill, 1991.

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Knecht, Ken. Advanced Turbo C. Scott, Foresman, 1989.

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Leventhal, Lance A. Turbo C quickstart. Microtrend Books, 1992.

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Book chapters on the topic "Turbo C++"

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Herrmann, Dietmar. "Der Turbo C-Compiler." In Effektiv Programmieren in C. Vieweg+Teubner Verlag, 1989. http://dx.doi.org/10.1007/978-3-322-83933-6_18.

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Herrmann, Dietmar. "Der Turbo C-Compiler." In Effektiv Programmieren in C. Vieweg+Teubner Verlag, 1991. http://dx.doi.org/10.1007/978-3-663-14170-9_18.

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Mockus, Jonas. "Turbo C Version (TCGM)." In Applied Optimization. Springer US, 2000. http://dx.doi.org/10.1007/978-1-4615-4671-9_5.

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Aupperle, Martin. "Die C++ Sprache." In Objektorientiert mit TURBO C++. Vieweg+Teubner Verlag, 1992. http://dx.doi.org/10.1007/978-3-322-93857-2_2.

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Aupperle, Martin. "C++ Teil 2." In Objektorientiert mit TURBO C++. Vieweg+Teubner Verlag, 1992. http://dx.doi.org/10.1007/978-3-322-93857-2_5.

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Aupperle, Martin. "C++ Teil 1 (Klassen)." In Objektorientiert mit TURBO C++. Vieweg+Teubner Verlag, 1992. http://dx.doi.org/10.1007/978-3-322-93857-2_3.

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Aupperle, Martin. "Warum objektorientierte Programmierung ?" In Objektorientiert mit TURBO C++. Vieweg+Teubner Verlag, 1992. http://dx.doi.org/10.1007/978-3-322-93857-2_1.

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Aupperle, Martin. "Virtuelle Funktionen." In Objektorientiert mit TURBO C++. Vieweg+Teubner Verlag, 1992. http://dx.doi.org/10.1007/978-3-322-93857-2_10.

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Aupperle, Martin. "Polymorphismus: Zwei Fallstudien." In Objektorientiert mit TURBO C++. Vieweg+Teubner Verlag, 1992. http://dx.doi.org/10.1007/978-3-322-93857-2_11.

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Aupperle, Martin. "Streams." In Objektorientiert mit TURBO C++. Vieweg+Teubner Verlag, 1992. http://dx.doi.org/10.1007/978-3-322-93857-2_12.

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Conference papers on the topic "Turbo C++"

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Hughes, Larry. "Teaching operating systems using Turbo C." In the twenty-third SIGCSE technical symposium. ACM Press, 1992. http://dx.doi.org/10.1145/134510.134547.

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Taylor, Alexander H., Pavan Naik, Simon Nibler, and Nisar Al-Hasan. "Optimization of Variable Geometry Turbine Electric Turbocharger for a Heavy-Duty, On-Highway Fuel Cell." In ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2023. http://dx.doi.org/10.1115/gt2023-101224.

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Abstract An air compressor is a necessary component on fuel cell electric generators as fuel cells do not pull in air without an external intervention. There are many fuel cell air compression options, each with their own benefits and drawbacks, such as roots-style screw compressors, radial e-compressors, e-turbos with wastegate, and e-turbos with a variable geometry turbine (VTG). Turbocharger turbine wheels for internal combustion engine applications are optimized to maximize exhaust gas enthalpy extraction while limiting centrifugal forces in the blades. In the presence of high temperature
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Walker, Megan, and Xiao Huang. "Isothermal Oxidation of René N5 at 1150°C." In ASME Turbo Expo 2018: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/gt2018-75078.

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In this study, single crystal superalloy René N5 was exposed in air at 1150 °C for up to 16 hours to evaluate the alloy’s short-term oxidation behaviour and the potential for developing a no-bond coat TBC system. The results showed that after 1 hour of exposure, a three layered oxide developed on the surface, consisting of spinel, Ta-containing oxide and alumina just above the substrate. After 4 hours of exposure, oxide spallation occurred; this became more pronounced after 16 hours. The oxide spallation took place between the top spinel layer and alumina layer, where Ta-rich oxide was more ab
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Chen, Hua, Yuchao Song, Aiguo Gu, Yangfang Zhang, and Hongwei Li. "Turbocharger Turbine Rotor Design for Low U/C Values." In ASME Turbo Expo 2019: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2019. http://dx.doi.org/10.1115/gt2019-90070.

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Abstract Emission regulations worldwide demand better low-end torque from internal combustion engines. This pushes the operating condition of turbocharger turbine to lower U/C values, where U is the blade tip speed and C is the turbine isentropic spouting velocity which increases with turbine expansion ratio. Traditional radial and some mixed flow turbines, dictated by their rotor design, have their efficiency peaks at U/C value around 0.70, a value considerably larger than desired. In this paper, we deliberate the measures to shift the peak efficiency of turbine rotor toward a lower U/C value
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Boestaman, Refrizal, V. P. Swaminathan, and H. L. Bernstein. "Protective Coatings and Degradation Experiences for First Stage Buckets on GE MS-5002B/C Gas Turbines." In ASME 1996 Turbo Asia Conference. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-ta-032.

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PT Arun operates 21 GE Model MS-5002 B/C gas turbines as mechanical drive with a total power of 514 MW, and a total of 2.7 million hours of accumulated operation. The first generations of simple cycle gas turbines were designed at 1700 F (927 C) firing temperature using first stage buckets design cast from IN-738LC and coated with a conventional 2-phase platinum aluminide coating (Pt-Al). Since 1989, the output power was increased by raising gas turbine firing temperature to 1770 F (965 C). This uprate was implemented by using first stage buckets cast from GTD-111 DS and coated with GT-29 Plus
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Cheng, W. Y., Y. Z. Robert Hu, and C. C. Wang. "Film Condensation of R-22 and R-410A on Horizontal Enhanced Tubes." In ASME 1997 Turbo Asia Conference. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/97-aa-032.

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This study experimentally investigates the film condensation of R-22 and R-410A on two horizontal enhanced tubes. The test tubes include a GEWA-C and a GEWA-TWX. Data was measured at three different saturation temperatures (35°C, 40°C and 45°C) in accordance with the range of practical condensation conditions in the air-conditioning and refrigeration applications. Average heat transfer coefficients were determined by overall heat transfer coefficients based on energy balance. The comparisons of heat transfer coefficients between R-22 and R-410A for both test tubes were presented.
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Boulanger, Andrew, John Hutchinson, Wing F. Ng, et al. "Experimental Based Empirical Model of the Initial Onset of Sand Deposits on Hastelloy-X From 1000°C to 1100°C Using Particle Tracking." In ASME Turbo Expo 2017: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gt2017-64480.

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Deposition experiments are performed on a Hastelloy-X coupon using Arizona Road Test Dust (ARD). A statistical empirical model of the initial onset of ARD deposits is developed from the experimental data. The initial onset of deposits are a quadratic function of local surface temperature and impact velocity components (normal and tangential). A prominent observation is that tangential impact velocity has a significant non-linear, independent effect on deposits relative to normal impact velocity and local surface temperatures. All experiments use 20–40 μm ARD on a bare metal surface over a 1000
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Wei, Wei, Weilin Zhuge, Yangjun Zhang, and Yongsheng He. "Comparative Study on Electric Turbo-Compounding Systems for Gasoline Engine Exhaust Energy Recovery." In ASME Turbo Expo 2010: Power for Land, Sea, and Air. ASMEDC, 2010. http://dx.doi.org/10.1115/gt2010-23204.

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Electric turbo-compounding system attracts more attention in recent years with the advance of electronic control devices. There are mainly three kinds of electric turbo-compounding systems for internal combustion engines: System A has an electric-assisted turbocharger, System B has a turbo-generator that is in series with the turbocharger, and System C has a turbo-generator that is in parallel with the turbocharger. A comparative study on the performance of these three kinds of systems for a 1.8L turbocharged gasoline engine is presented. The comparative study has been carried out using 1D sim
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Hansen, Mogens Weel, and Jan Sandvig Nielsen. "Optimal Integration of Humid Air Cycle in Energy Intensive Industries." In ASME 1996 Turbo Asia Conference. American Society of Mechanical Engineers, 1996. http://dx.doi.org/10.1115/96-ta-049.

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Humid Air Turbine cycle (HAT) is characterised by its high single cycle efficiency. The HAT cycle is typically constrained by a pinch point at low temperature. This indicates that additional heat in the range 100 °C to 200 °C can be utilised with high marginal efficiency. At the same time energy intensive industries (for example refineries, Cement production plants and Steel works) typically have a surplus of heat from around 250 °C to 300 °C and down. This study is aimed at the integration of HAT Cycle into the industrial process plant where the complementary features can be exploited. The pr
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Pint, Bruce A., Rishi Pillai, and James R. Keiser. "Effect of Supercritical CO2 on Steel Ductility at 450°-650°C." In ASME Turbo Expo 2021: Turbomachinery Technical Conference and Exposition. American Society of Mechanical Engineers, 2021. http://dx.doi.org/10.1115/gt2021-59383.

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Abstract The compatibility of ferritic-martensitic (FM) and conventional and advanced austenitic steels with supercritical CO2 (sCO2) is being explored at 450°–650°C to determine their maximum temperature capability. In addition to measuring reaction kinetics and reaction product thickness, bulk carbon content and post-exposure room temperature tensile properties were assessed by exposing both alloy coupons and 25 mm long dogbone tensile specimens. After 1–2 kh exposures in 300 bar research grade (RG) sCO2, ∼9 and 12%Cr FM steels had similar behavior under these conditions. Consistent with the
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Reports on the topic "Turbo C++"

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ตั้งชวาล, สง่า. การประเมินเสถียรภาพของเหมืองเปิดและอุโมงค์ใต้ดิน : รายงาน. จุฬาลงกรณ์มหาวิทยาลัย, 1995. https://doi.org/10.58837/chula.res.1995.26.

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การประเมินเสถียรภาพของเหมืองเปิด และอุโมงค์ใต้ดิน สามารถนำไปประยุกต์ใช้กับงานเปิดหน้าดิน/หิน งานระเบิดเหมืองหิน และการขุดเจาะอุโมงค์ใต้ดิน เกณฑ์ที่ใช้ในการกำหนดสำหรับการวิเคราะห์เสถียรภาพโครงการที่อยู่ในขั้นวางแผน ก่อนดำเนินการโดยใช้ค่าปัจจัยของความปลอดภัย (factor of safety) และกำหนดให้จุดที่สมดุลเชิงสถิตย์ศาสตร์ มีค่าปัจจัยของความปลอดภัยเท่ากับ หนึ่ง การประเมินเสถียรภาพของเหมืองเปิด และอุโมงค์ใต้ดินแบ่งงานการวิเคราะห์ออกเป็นหลายชนิด หลายวิธีการและหลายรูปแบบ ได้แก่ การพังทลายแนวระนาบ การพังทลายรูปวงกลม (สลิป) การพังทลายรูปลิ่ม การพังทลายแบบทอปเปิล สำหรับส่วนของงานวิเคราะห์นี้ ผู้วิจัยได้อ้างอิ
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