Relevant bibliographies by topics / Aerodynamic pressure

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Book chapters
  5. Conference papers
  6. Reports

Academic literature on the topic 'Aerodynamic pressure'

Author: Grafiati
Published: 4 June 2021
Last updated: 25 July 2025

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Journal articles on the topic "Aerodynamic pressure"

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Xie, Dan, Min Xu, Honghua Dai, and Tao Chen. "New Look at Nonlinear Aerodynamics in Analysis of Hypersonic Panel Flutter." Mathematical Problems in Engineering 2017 (2017): 1–13. http://dx.doi.org/10.1155/2017/6707092.

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A simply supported plate fluttering in hypersonic flow is investigated considering both the airflow and structural nonlinearities. Third-order piston theory is used for nonlinear aerodynamic loading, and von Karman plate theory is used for modeling the nonlinear strain-displacement relation. The Galerkin method is applied to project the partial differential governing equations (PDEs) into a set of ordinary differential equations (ODEs) in time, which is then solved by numerical integration method. In observation of limit cycle oscillations (LCO) and evolution of dynamic behaviors, nonlinear ae
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Qi, Xiaojing, Yuxin Ou, Hance Zhang, and Da Wang. "Efficiency Enhancement Design Approach in the Side Wing of a FSAE Car Utilizing a Shutter-Like Fairing Structure." Applied Sciences 12, no. 13 (2022): 6552. http://dx.doi.org/10.3390/app12136552.

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Aerodynamical design is one of the critical technologies in race car engineering, and favorable race car aerodynamics is supposed to provide sufficient negative lift force and keep the center of pressure in the vicinity of center of mass. Taking the Formula Society of Automotive Engineers (FSAE) cars as an example, side wing structure is frequently adopted for better grip in the mid-back of short wheelbase, open wheel race cars. This research designs a shutter-like fairing structure and utilizes it to weaken the vorticity and reinforce the pressure of side wing flow field. The sensitivity of s
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Jing, Haiquan, Xiaoyu Ji, Xuhui He, Shifeng Zhang, Jichao Zhou, and Haiyu Zhang. "Dynamic Characteristics of Unsteady Aerodynamic Pressure on an Enclosed Housing for Sound Emission Alleviation Caused by a Passing High-Speed Train." Applied Sciences 12, no. 3 (2022): 1545. http://dx.doi.org/10.3390/app12031545.

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Train speed is increasing due to the development of high-speed railway technology. However, high-speed trains generate more noise and discomfort for residents, enclosed housing for sound emission alleviation is needed to further reduce noise. Because these enclosed housings for sound emission alleviation restrain the air flow, strong and complicated aerodynamic pressures are generated inside the housing for sound emission alleviation when a train passes through at a high speed. This train-induced aerodynamic pressure, particularly its dynamic characteristics, is a key parameter in structural d
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Junaidin, Buyung. "AERODYNAMIC ANALYSIS OF SPORT UTILITY VEHICLE (SUV) BY COMPUTATIONAL FLUID DYNAMICS (CFD) APROACH." Vortex 3, no. 1 (2022): 67. http://dx.doi.org/10.28989/vortex.v3i1.1161.

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The main purpose of aerodynamics analysis of a vehicle is optimizing it’s form to increase aerodynamics efficiency. More streamline of aerodynamic design of a vehicle not just effecting to lower fuel consumption which is cause by lower drag due to wind at highspeed, but also increasing stability dan control of the vehicle itself. The vehicles are existed with many variations of form so they have difference aerodynamic characteristics. For a personal vehicle like cars, have many variants such as sedan, sport utility vehicle (SUV), multipurposes utility vehicle (MPV), ect. It becomes a motivatio
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Zhang, Cheng Chun, Wen Qiang Wang, Lei Shi, Jing Wang, and Lu Quan Ren. "Experimental and Numerical Study on Aerodynamic Noise Reduction of Cylindrical Rod with Bionic Wavy Surface." Applied Mechanics and Materials 461 (November 2013): 690–701. http://dx.doi.org/10.4028/www.scientific.net/amm.461.690.

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Inspired by the non-smooth structure of the leading edge of owls wing,a bionic wavy cylindrical surface is proposed in this paper to reduce the aerodynamic noise of a cylindrical rod. The effects of bionic wavy surface on the aerodynamic and aeroacoustic performance of the cylinder are investigated by wind tunnel and numerical simulation. The fluctuating pressure of the smooth cylinder and the bionic wavy surface cylinder are tested by pulsating pressure sensors in FD-09 low speed wind tunnel of China Aerospace Aerodynamics Research Institute. The fluctuating pressure of the bionic wavy surfac
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Sun, Xiaoqi, and Han Xiao. "Numerical Modeling and Investigation on Aerodynamic Noise Characteristics of Pantographs in High-Speed Trains." Complexity 2018 (2018): 1–12. http://dx.doi.org/10.1155/2018/6932596.

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Pantographs are important devices on high-speed trains. When a train runs at a high speed, concave and convex parts of the train cause serious airflow disturbances and result in flow separation, eddy shedding, and breakdown. A strong fluctuation pressure field will be caused and transformed into aerodynamic noises. When high-speed trains reach 300 km/h, aerodynamic noises become the main noise source. Aerodynamic noises of pantographs occupy a large proportion in far-field aerodynamic noises of the whole train. Therefore, the problem of aerodynamic noises for pantographs is outstanding among m
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Quan, Vu Hai. "RESEARCH AND OPTIMIZATION OF SPORT UTILITY VEHICLE AERODYNAMIC DESIGN." Applied Engineering Letters : Journal of Engineering and Applied Sciences 9, no. 2 (2024): 105–15. http://dx.doi.org/10.46793/aeletters.2024.9.2.5.

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Drag and lift are two important parameters to evaluate a vehicle’s aerodynamic performance. Aerodynamic resistance (drag force Fd) prevents the movement of the vehicle and has a value proportional to the square of the velocity. That is, when the speed increases twice, the aerodynamic drag will increase fourfold. This article presents a plan to design a sport utility vehicle model with improved aerodynamics by using Ansys Fluent software to analyze pressure distribution areas that affect aerodynamics and the body. Based on the results obtained, the areas of stress and maximum pressure concentra
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Metar, Manas. "Aerodynamic Analysis of Spoiler at Varying Speeds and Angles." International Journal for Research in Applied Science and Engineering Technology 9, no. 11 (2021): 526–35. http://dx.doi.org/10.22214/ijraset.2021.38843.

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Abstract: Spoilers have been there in practice since years for the purpose of improving aerodynamics of a car. The pressure drag created at the end of the vehicle, referred to as wake region affects handling of the vehicle. This could be hazardous for the cars at high speeds. By adding a spoiler to the rear of the car reduces that pressure drag and the enhanced downforce helps in better traction. The paper presents aerodynamic analysis of a spoiler through Computational Fluid Dynamics analysis. The spoiler is designed using Onshape software and analyzed through SIMSCALE software. The simulatio
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Ben Mosbah, A., R. M. Botez, and T. M. Dao. "New methodology combining neural network and extended great deluge algorithms for the ATR-42 wing aerodynamics analysis." Aeronautical Journal 120, no. 1229 (2016): 1049–80. http://dx.doi.org/10.1017/aer.2016.46.

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ABSTRACTThe fast determination of aerodynamic parameters such as pressure distributions, lift, drag and moment coefficients from the known airflow conditions (angles of attack, Mach and Reynolds numbers) in real time is still not easily achievable by numerical analysis methods in aerodynamics and aeroelasticity. A flight parameters control system is proposed to solve this problem. This control system is based on new optimisation methodologies using Neural Networks (NNs) and Extended Great Deluge (EGD) algorithms. Validation of these new methodologies is realised by experimental tests using a w
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Zhang, Ying Chao, Zhe Zhang, Shuang Hu Luo, and Jian Hua Tian. "Aerodynamic Numerical Simulation in the Process of Car Styling." Applied Mechanics and Materials 16-19 (October 2009): 862–65. http://dx.doi.org/10.4028/www.scientific.net/amm.16-19.862.

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With the development of automotive industry of China, more and more new cars are brought out. Then more and more stylists and engineers will take part in car styling to design new car. In the process of car styling, Car aerodynamics is important to its performance. Especially for more excellent handling and stability performance, more aerodynamic analysis and optimization should been done. At first it was introduced that the process of car styling in this paper. The functions of aerodynamics in the process were indicated. Secondly some ways of aerodynamic analysis were put forward. The first o
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Dissertations / Theses on the topic "Aerodynamic pressure"

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Gonçalves, Duarte. "Aerodynamic study of atmospheric-pressure plasma jets." Electronic Thesis or Diss., université Paris-Saclay, 2024. http://www.theses.fr/2024UPASP101.

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Les jets de plasma à pression atmosphérique (JPPAs) étendent le plasma au-delà des parois d'un réacteur. Ces sources de plasma produisent et délivrent des espèces réactives à des matériaux sensibles. En conséquence, les JPPAs ont de nombreuses applications en biologie, médecine, analyse chimique et traitement des matériaux. Les JPPAs sont produits par le passage répétitif d'ondes d'ionisation (OI), guidées en aval par l'écoulement. À leur tour, les OI perturbent l'écoulement à chaque passage. L'étude de l'aérodynamique des JPPAs offre un chemin pour comprendre le couplage plasma-écoulement. Da
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BIGANZOLI, ILARIA. "Characterization of atmospheric pressure plasmas for aerodynamic applications." Doctoral thesis, Università degli Studi di Milano-Bicocca, 2014. http://hdl.handle.net/10281/53249.

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The use of plasmas in aerodynamics has become a recent topic of interest. In particular, over the last ten years, plasma actuation has received much attention as a promising active method for airflow control. Flow control consists of manipulating the properties of a generic moving fluid with the aim of achieving a desired change, but flow dynamics in proximity of a solid object is usually considered, being a consistent and significant issue in many engineering applications, such as engine, automobile or airplane design. Plasma control of airflows along surfaces has been the subject of several
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Bamberger, Konrad [Verfasser]. "Aerodynamic Optimization of Low-Pressure Axial Fans / Konrad Bamberger." a : Shaker, 2015. http://d-nb.info/1080762191/34.

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Holmberg, Eva. "Aerodynamic measurements of normal voice." Doctoral thesis, Stockholms universitet, Institutionen för lingvistik, 1993. http://urn.kb.se/resolve?urn=urn:nbn:se:su:diva-40215.

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Vocal fold vibration results from an alternating balance between subglottal air pressure that drives the vocal folds apart and muscular, elastic, and restoring forces that draw them together. The aim of the present thesis is to present quantitative data of normal vocal function using a noninvasive method. Measurements are made on the inverse filtered airflow waveform, of estimated average trans glottal pressure and glottal airflow, and of sound pressure for productions of syllable sequences. Statistical results are used to infer mechanisms that underlie differences across ( 1 ) normal, loud, a
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Grodek, Kristen Ashley. "The Effect of Sound Pressure Level Variation on Aerodynamic Measures." Miami University / OhioLINK, 2009. http://rave.ohiolink.edu/etdc/view?acc_num=miami1239321162.

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Rossetti, Alessandro <1977&gt. "Design and development of new pressure sensors for aerodynamic applications." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2008. http://amsdottorato.unibo.it/787/1/Tesi_Rossetti_Alessandro.pdf.

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This artwork reports on two different projects that were carried out during the three years of Doctor of the Philosophy course. In the first years a project regarding Capacitive Pressure Sensors Array for Aerodynamic Applications was developed in the Applied Aerodynamic research team of the Second Faculty of Engineering, University of Bologna, Forlì, Italy, and in collaboration with the ARCES laboratories of the same university. Capacitive pressure sensors were designed and fabricated, investigating theoretically and experimentally the sensor’s mechanical and electrical behaviours by means of
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Rossetti, Alessandro <1977&gt. "Design and development of new pressure sensors for aerodynamic applications." Doctoral thesis, Alma Mater Studiorum - Università di Bologna, 2008. http://amsdottorato.unibo.it/787/.

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This artwork reports on two different projects that were carried out during the three years of Doctor of the Philosophy course. In the first years a project regarding Capacitive Pressure Sensors Array for Aerodynamic Applications was developed in the Applied Aerodynamic research team of the Second Faculty of Engineering, University of Bologna, Forlì, Italy, and in collaboration with the ARCES laboratories of the same university. Capacitive pressure sensors were designed and fabricated, investigating theoretically and experimentally the sensor’s mechanical and electrical behaviours by means of
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Garrison, Courtney Rollins. "Repeatability of Aerodynamic Measurements of Voice." Miami University / OhioLINK, 2009. http://rave.ohiolink.edu/etdc/view?acc_num=miami1239309229.

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Yoon, Sungho. "Advanced aerodynamic design of the intermediate pressure turbine for aero-engines." Thesis, University of Cambridge, 2010. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.608551.

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Wang, Yifei. "Experimental Study of Wheel-Vehicle Aerodynamic Interactions." Thesis, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique, 2019. http://www.theses.fr/2019ESMA0002/document.

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Sur une maquette à l’échelle 2/5ième équipée d’un diffuseur et de pneus Michelin. La géométrie du véhicule, basée sur le modèle ASMO, a été modifiée précédemment à ce travail afin d’obtenir un angle d’attaque de l’écoulement sur les roues avant et un équilibre du sillage réaliste en présence de quatre roues tournantes. Cette configuration a servi de référence dans le cadre de cette étude.Il a été mis en évidence que la configuration de base avec un sillage équilibré peut facilement être modifiée d’un point de vue aérodynamique en changeant l’état des roues (en rotation ou pas) et le type de pn
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Books on the topic "Aerodynamic pressure"

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K, Notestine Kristopher, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Aerodynamic pressure and heating-rate distributions in tile gaps around chine regions with pressure gradients at a Mach number of 6.6. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

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Moshasrov, V. Luminescent pressure sensors in aerodynamic experiments. CWA 22 Corporation, 1998.

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H, Ricketts Rodney, Hess R. W, and Langley Research Center, eds. Recent transonic unsteady pressure measurements at the NASA Langley Research Center. National Aeronautics and Space Administration, Langley Research Center, 1985.

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Schuster, D. M. Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel. National Aeronautics and Space Administration, Langley Research Center, 2001.

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E, Mineck Raymond, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Aerodynamic characteristics and pressure distributions for an executive-jet baseline airfoil section. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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Nemec, Marian. Aerodynamic computations using the convective upstream split pressure scheme with local preconditioning. Dept. of Aerospace Science and Engineering, University of Toronto, 1998.

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Nemec, Marian. Aerodynamic computations using the convective upstream split pressure scheme with local preconditioning. National Library of Canada, 1998.

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Labrujere, Th E. Correction for wall interference in a solid-wall wind tunnel using sparse measured boundary conditions. National Aerospace Laboratory, 1989.

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United States. National Aeronautics and Space Administration., ed. IPAC--Inlet Performance Analysis Code. National Aeronautics and Space Administration, 1997.

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United States. National Aeronautics and Space Administration., ed. IPAC--Inlet Performance Analysis Code. National Aeronautics and Space Administration, 1997.

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Book chapters on the topic "Aerodynamic pressure"

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Decher, Reiner. "The Compressor: Gas Turbine Engine Keystone." In The Vortex and The Jet. Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_10.

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AbstractAll engines involve the raising of pressure in the engine’s medium, be it liquid compression of water, piston-cylinder compression of air or compression by aerodynamic forces. The last is the hardest because it is required to be efficient and stable. An aerodynamic air compressor works by slowing velocities to raise pressure. The airfoil has a difficult time doing this reliably and well and so does the compressor. When it does, it allows for amazing performance of the engine in terms of power and efficiency.
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Paluch, B. "Light transmission control technique and correlation with pressure loss characteristics of perforated panels for Hybrid Laminar Flow Applications." In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-540-45359-8_9.

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Ellis, J. E., S. A. Walsh, and D. I. A. Poll. "Assessment of the eN Method as a Transition Prediction Tool for Zero Pressure Gradient Flows with and without Boundary Layer Suction." In Aerodynamic Drag Reduction Technologies. Springer Berlin Heidelberg, 2001. http://dx.doi.org/10.1007/978-3-540-45359-8_34.

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Hölscher, N., and H. J. Niemann. "Non-Parametric Identification of a Multiple Aerodynamic Pressure Admittance." In Notes on Numerical Fluid Mechanics (NNFM). Vieweg+Teubner Verlag, 1993. http://dx.doi.org/10.1007/978-3-663-13986-7_30.

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Liu, Kaihe, Haitao Chang, and Yang Li. "Some Thoughts About the Aerodynamic Pressure Center of Automobile." In Lecture Notes in Electrical Engineering. Springer Nature Singapore, 2024. http://dx.doi.org/10.1007/978-981-97-0252-7_48.

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Chang, Hong-Bin, Uzu-Kuei Hsu, Yao-Yu Tsai, Chen-Yu Wu, and Cheng-Hsien Tai. "Aerodynamic Analysis and Application of High-Pressure Air Gun." In Advanced Structured Materials. Springer Nature Switzerland, 2025. https://doi.org/10.1007/978-3-031-84346-4_27.

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Huang, Thomas T., and Ming-Shun Chang. "Computation of Velocity and Pressure Variation Across Axisymmetric Thick Turbulent Stern Flows." In Numerical and Physical Aspects of Aerodynamic Flows III. Springer New York, 1986. http://dx.doi.org/10.1007/978-1-4612-4926-9_19.

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Zharkova, G. M., A. I. Maksimov, A. A. Pavlov, and V. M. Khachaturyan. "Pressure Visualization on Aerodynamic Surface by the Method of Luminescent Coating." In Flow Visualization VI. Springer Berlin Heidelberg, 1992. http://dx.doi.org/10.1007/978-3-642-84824-7_109.

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Usherwood, James R. "The aerodynamic forces and pressure distribution of a revolving pigeon wing." In Animal Locomotion. Springer Berlin Heidelberg, 2010. http://dx.doi.org/10.1007/978-3-642-11633-9_33.

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Wu, Meng-ling, Yang-yong Zhu, Chun Tian, and Wei-wei Fei. "Influence of Aerodynamic Braking on the Pressure Wave of a Crossing High-Speed Train." In China's High-Speed Rail Technology. Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-5610-9_8.

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Conference papers on the topic "Aerodynamic pressure"

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CARVER, D., W. WARD, and M. BYERS. "Continuous sweep pressure prediction technique." In 14th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-767.

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Birkenstock, David. "Increased Fuel Economy From Powered Aerodynamics and Aerodynamic Pressure Thrust." In 18th AIAA Lighter-Than-Air Systems Technology Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-2864.

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STAINBACK, P., R. MCGHEE, W. BEASLEY, and H. MORGAN, JR. "The Langley Research Center's Low-Turbulence Pressure Tunnel." In 14th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-762.

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MORRIS, M., J. DONOVAN, J. KEGELMAN, S. SCHWAB, R. LEVY, and R. CRITES. "Aerodynamic applications of pressure-sensitive paint." In 30th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-264.

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FUNG, Y. T., G. SETTLES, and A. RAY. "Microprocessor control of high-speed wind tunnel stagnation pressure." In 15th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-2062.

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SMELTZER, D., and A. LEVIN. "Evaluation of an electronic scanner of pressure (ESOP) module." In 14th Aerodynamic Testing Conference. American Institute of Aeronautics and Astronautics, 1986. http://dx.doi.org/10.2514/6.1986-771.

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Larsen, Allan. "Horizontal Aerodynamic Derivatives in Bridge Flutter Analysis." In ASME 2014 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/pvp2014-28251.

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Inclusion of a horizontal degree of freedom along with the vertical and twisting degrees of freedom has been an active area of research in bridge flutter predictions for the past three decades. While much work has been published on theoretical aspects, limited experience as to the importance of the horizontal degree of freedom is available in the literature. Three cases of actual long span bridge designs are examined with respect to the critical wind speed for onset of classical flutter. For the tree cases examined inclusion of the horizontal modes of motion had almost negligible influence on
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CHUNG, KUNG-MING, and FRANK LU. "Shock-tube calibration of a fast-response pressure transducer." In 16th Aerodynamic Ground Testing Conference. American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-1399.

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Chang, Y. B., and P. M. Moretti. "Aerodynamic Characteristics of Pressure-Pad Air Bars." In ASME 1997 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 1997. http://dx.doi.org/10.1115/imece1997-0091.

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Abstract Air flotation ovens are widely used for non-contact support and drying of coated papers and plastic films (generically called webs). The main components in air flotation ovens are air bars which have slot nozzles through which hot air jets are ejected. Problems in air flotation drying techniques include sideward motion of the web, web flutter, and contact between the web and air bars. The key to analyzing these problems is to determine the aerodynamic forces on the web. This paper discusses the aerodynamic forces generated by pressure-pad type air bars, each of which has two slot nozz
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Zolotarev, Igor, Václav Vlček, and Jan Kozánek. "Unsteady Aerodynamic Forces Measured on a Fluttering Profile." In ASME 2014 Pressure Vessels and Piping Conference. American Society of Mechanical Engineers, 2014. http://dx.doi.org/10.1115/pvp2014-28567.

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The study presents evaluation of optical measurements of the air flow field near the fluttering profile NACA0015 with two-degrees of freedom, Mach number of the flutter occurrence were M=0.21 and M=0.45. Aerodynamic forces (drag and lift components) were evaluated independently on the upper and lower surfaces of the profile. Using the mentioned decomposition, the new information about mechanism of flutter properties was obtained. The forces on the upper and lower surfaces are phase shifted and are partially eliminated as a result of the circulation around the profile. The cycle changes of thes
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Reports on the topic "Aerodynamic pressure"

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Aerodynamic Development of the GAC ENO.146 Concept. SAE International, 2021. http://dx.doi.org/10.4271/2021-01-5093.

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This paper describes the aerodynamic development process and features of the flow field of the GAC ENO.146, a concept vehicle shown in Guangzhou Auto Show 2019, which achieved a CD of 0.146. Key factors in the design process, including how design decisions are made and how the interactions occur between aerodynamicists and designers are explained in detail. The design language forms the next generation of BEVs. The aerodynamic development philosophy is guided by three principles: minimizing flow separation, maximizing rear pressure recovery, and controlling tire wake. This vehicle took full ad
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