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Relevant bibliographies by topics / Wind tunnels – Design

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Academic literature on the topic 'Wind tunnels – Design'

Author: Grafiati

Published: 4 June 2021

Last updated: 11 February 2022

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Journal articles on the topic "Wind tunnels – Design"

1

Hrúz, Michal, Pavol Pecho, and Martin Bugaj. "Design procedure and honeycomb screen implementation to the air transtport department’s subsonic wind tunnel." AEROjournal 16, no. 2 (2020): 3–8. http://dx.doi.org/10.26552/aer.c.2020.2.1.

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Wind tunnels are the most widely used tools when comes to validation of Reynold number. Most of wind tunnels use various air straighteners or flow conditioners to achieve as most unified air flow as it’s possible. This article deals with design and creation procedure of air flow straightener – honeycomb screen. Based on mathematical relations and empirical experience defines dimensions and characteristics for subsonic wind tunnel of the Air Transport Department of University of Žilina. Wind tunnel equipped with a suitable screen provides more relevant and accurate data, which are crucial for f

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Govinda Raju, S. P. "Role of wind tunnels in aircraft design." Resonance 8, no. 1 (2003): 72–76. http://dx.doi.org/10.1007/bf02834452.

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Wiriadidjaja, Surjatin, Fadilah Hasim, Shuhaimi Mansor, Waqar Asrar, Azmin Shakrine Mohd Rafie, and Ermira Junita Abdullah. "Subsonic Wind Tunnels in Malaysia: A Review." Applied Mechanics and Materials 225 (November 2012): 566–71. http://dx.doi.org/10.4028/www.scientific.net/amm.225.566.

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In Malaysia, there exist wind tunnels operated by several universities and organizations. Most of them are actively used for a variety of experimental works that are needed by uncounted educational curricula and aerodynamics related researches. Lately, wind tunnels have even become increasingly accepted as one of common engineering tools in solving of unexpected and abundant wind engineering problems that are continually facing automotive industries, oil and gas companies, as well as governmental agencies and ministries. This paper is meant to present an overview of the existing wind tunnels,

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Flamand, Olivier, Philippe Delpech, Pierre Palier, and Jean-Paul Bouchet. "Benefit of Wind Tunnels with Large Test Sections for Wind Engineering Applications." Mathematical Modelling in Civil Engineering 15, no. 2 (2019): 14–19. http://dx.doi.org/10.2478/mmce-2019-0005.

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Abstract Atmospheric Boundary layer wind tunnels (ABLWT) dedicated to building safety and comfort have been operated by CSTB in Nantes since 1971. Because ABLWT only deal with reduced scale models of real structures, the necessity of a larger wind tunnel, the Jules Verne Climatic wind tunnel (CWT), able to reproduce extreme wind loads on real scale structures arose in the years 80. Hence, it became a major European facility operating for improvement of the safety, quality and environmental impact of buildings and civil engineering works as well as products from industrial fields (transportatio

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Floratou, Avrilia, Frank Bertsch, Jignesh M. Patel, and Georgios Laskaris. "Towards building wind tunnels for data center design." Proceedings of the VLDB Endowment 7, no. 9 (2014): 781–84. http://dx.doi.org/10.14778/2732939.2732950.

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Liu, Shanhe, Zhiwen Luo, Keer Zhang, and Jian Hang. "Natural Ventilation of a Small-Scale Road Tunnel by Wind Catchers: A CFD Simulation Study." Atmosphere 9, no. 10 (2018): 411. http://dx.doi.org/10.3390/atmos9100411.

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Providing efficient ventilation in road tunnels is essential to prevent severe air pollution exposure for both drivers and pedestrians in such enclosed spaces with heavy vehicle emissions. Longitudinal ventilation methods like commercial jet fans have been widely applied and confirmed to be effective for introducing external fresh air into road tunnels that are shorter than 3 km. However, operating tunnel jet fans is energy consuming. Therefore, for small-scale (~100 m–1 km) road tunnels, mechanical ventilation methods might be highly energetically expensive and unaffordable. Many studies have

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Belostotsky, Alexander, Pavel Akimov, and Irina Afanasyeva. "ABOUT “LEGITIMIZATION” OF NUMERICAL MODELLING OF WIND IMPACTS ON BUILDINGS AND STRUCTURES IN DESIGN CODES." International Journal for Computational Civil and Structural Engineering 15, no. 4 (2019): 14–24. http://dx.doi.org/10.22337/2587-9618-2019-15-4-14-24.

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The distinctive paper is detoded to problem of “legitimization” of numerical modelling of wind loads and impacts on buildings and structures. General information about computational fluid dynamics (CFD) and its development prospects is presented. The main advantages and disadvantages of numerical simulation compared with tests in wind tunnels (wind tunnel tests) are considered. Besides, information about the second modification of corresponding Russian design codes (SP 20.13330.2016 “SNiP 2.01.07-85* Loads and effects”) is provided. Prospects for the further development of numerical modelling

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Guo. "A Review of the Hydraulic Transient and Dynamic Behavior of Hydropower Plants with Sloping Ceiling Tailrace Tunnels." Energies 12, no. 17 (2019): 3220. http://dx.doi.org/10.3390/en12173220.

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The sloping ceiling tailrace tunnel is a novel tailrace tunnel system for hydropower plants. The design, operation, and maintenance of hydropower plants with sloping ceiling tailrace tunnels are based on the calculation and analysis of hydraulic transients and dynamic behavior. Research achievements have provided guidance and a basis for the safe, stable, and efficient operation of hydropower plants with sloping ceiling tailrace tunnels. Based on research achievements, sloping ceiling tailrace tunnels have been applied to more and more hydropower plants. This review paper gives a systematic li

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Wu, Hao, Yujian Zhong, Wei Xu, Wangshuaiyin Shi, Xinghao Shi, and Tong Liu. "Experimental Investigation of Ground and Air Temperature Fields of a Cold-Region Road Tunnel in NW China." Advances in Civil Engineering 2020 (July 22, 2020): 1–13. http://dx.doi.org/10.1155/2020/4732490.

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To fully understand the temperature distribution of cold regions and the variation law of temperature fields in cold-region tunnels, this paper presents a case-history study on a tunnel located on the eastern Qinghai-Tibet Plateau, China. The conclusion is as follows: the temperature outside the tunnel and the ambient temperature are affected by wind speed and light. The law of the temperature field in the tunnel is greatly affected by wind speed and wind direction. According to the field test, the wind speed in the tunnel is about 2.8 m/s in winter, and the daily average temperature at the ex

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Vukovic, Djordje, and Dijana Damljanovic. "Thermal effects influencing measurements in a supersonic blowdown wind tunnel." Thermal Science 20, no. 6 (2016): 2101–12. http://dx.doi.org/10.2298/tsci160404175v.

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During a supersonic run of a blowdown wind tunnel, temperature of air in the test section drops which can affect planned measurements. Adverse thermal effects include variations of the Mach and Reynolds numbers, variation of airspeed, condensation of moisture on the model, change of characteristics of the instrumentation in the model, et cetera. Available data on thermal effects on instrumentation are pertaining primarily to long-run-duration wind tunnel facilities. In order to characterize such influences on instrumentation in the models, in short-run-duration blowdown wind tunnels, temperatu

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Dissertations / Theses on the topic "Wind tunnels – Design"

1

Chui, Kwok-Lun. "Integrated wind tunnel based response analysis and structural optimization for serviceability design of tall buildings /." View abstract or full-text, 2004. http://library.ust.hk/cgi/db/thesis.pl?CIVL%202004%20CHUI.

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Thesis (M. Phil.)--Hong Kong University of Science and Technology, 2004.<br>Includes bibliographical references (leaves 187-194). Also available in electronic version. Access restricted to campus users.

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Szleper, Michele Lee. "Converging nozzle design for a subsonic wind tunnel to test heat sinks under impinging and parallel airflows." Thesis, Georgia Institute of Technology, 2002. http://hdl.handle.net/1853/17124.

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Blanco, Mark Richard. "Design and Qualification of a Boundary-Layer Wind Tunnel for Modern CFD Validation Experiments." Youngstown State University / OhioLINK, 2019. http://rave.ohiolink.edu/etdc/view?acc_num=ysu1559237473563483.

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Zucchini, Davide. "Design and realization of an instantaneous concentration measurement system for wind tunnel applications." Master's thesis, Alma Mater Studiorum - Università di Bologna, 2021. http://amslaurea.unibo.it/23540/.

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The aim of this project work is the design and realization of an instantaneous concentration measurement system to be used with binary gas mixtures. The design is focused on the simplicity of the set up and on its compactness, and it is specifically intended to be used in wind tunnel applications. The outcome of the design process for the specified system is an aspirating hot-wire probe based on a polypropylene 3D printed body and a simple single wire sensor. Specifically, a 3D printing machine based on the Material Jetting (MJ) technology was used for the probe manufacturing. One of the most

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Barnhart, Samuel. "Design and Development of a Coherent Detection Rayleigh Doppler Lidar System for Use as an Alternative Velocimetry Technique in Wind Tunnels." University of Dayton / OhioLINK, 2020. http://rave.ohiolink.edu/etdc/view?acc_num=dayton1595276402371536.

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Paula, Adson Agrico de. "The airfoil thickness effects on wavy leading edge phenomena at low Reynolds number regime." Universidade de São Paulo, 2016. http://www.teses.usp.br/teses/disponiveis/3/3150/tde-27092016-153422/.

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Recently, the wavy leading edge airfoils, inspired by the humpback whale´s flipper, have been investigated, as flow control mechanisms, at low Reynolds numbers in order to improve aerodynamic performance in this particular flow regime. The overall aim of this work is to investigate the airfoil geometric effects on wavy leading edge phenomena in the low Reynolds number regime. Experimental investigations were carried out correlating force measurements with mini-tuft and oil visualizations in order to understand the airfoil thickness effects on wavy leading edge phenomena. Three sets of airfoil

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Mallor, Fermin. "Enabling high-fidelity measurements of turbulent boundary layer flow over wing sections in the MTL wind tunnel." Thesis, KTH, Mekanik, 2019. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-264842.

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A reinforced fiber-glass model of a NACA 4412 wing profile is designed and set-up in the Minimum Turbulence Level (MTL) wind tunnel facility at KTH. The model has 65 pressure taps orifices, and the set-up includes two mounting panels designed to allow for particle image velocimetry (PIV) and hot wire anemometry (HWA) measurements of the boundary layer (to be performed in a future campaign). In a first experimental campaign pressure scans are conducted at three angles of attack of interest (5,10 and 12 degrees), and at four different Reynolds numbers based on chord length and inflow velocity (2

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Al-Qahtani, Turki Haif. "An improved design of wind towers for wind induced natural ventilation." Thesis, University of Bath, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.323566.

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Hamilton, Christianne Rhea. "Design of Test Sections for a High Enthalpy Wind Tunnel." MSSTATE, 2003. http://sun.library.msstate.edu/ETD-db/theses/available/etd-04082003-114126/.

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This document describes the design of a supersonic and a subsonic test section for a high enthalpy wind tunnel. A streamline is tracked through a supersonic test section using the method of characteristics. The specifics of the design program and the design techniques are illustrated for the supersonic section. The section of the paper dealing with the subsonic nozzle has a greatly diverse nature. This section details the inlet and exhaust restrictions and construction elements for the entire low speed system. The system is currently being set up for testing with the subsonic section, and the

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Carey, P. S. "Direct wind tunnel modelling of natural ventilation for design purposes." Thesis, University of Nottingham, 2004. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.422325.

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Books on the topic "Wind tunnels – Design"

1

Bell, James H. Contraction design for small low-speed wind tunnels. Stanford University, Department of Aeronautics and Astronautics, 1988.

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2

Watmuff, J. H. Design of a new contraction for the ARL low speed wind tunnel (U). Aeronautical Research Laboratories, 1986.

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Bell, James H. Design and calibration of the mixing layer and wind tunnel. Stanford University, Dept. of Aeronautics and Astronautics, 1989.

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Bell, J. H. Contraction design for small low-speed wind tunnels. National Aeronautics and Space Administration, 1988.

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5

Soderman, Paul T. The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1992.

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Soderman, Paul T. The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1992.

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Soderman, Paul T. The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1992.

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Soderman, Paul T. The design of test-section inserts for higher speed aeroacoustic testing in the Ames 80- by 120-foot wind tunnel. National Aeronautics and Space Administration, Ames Research Center, 1992.

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9

Schneider, Steven P. A quiet flow Ludwieg tube for study of transition in compressible boundary layers: Design and feasibility. School of Aeronautics and Astronautics, Purdue University, 1991.

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Hannemann, Klaus. Design of an axisymmetric, contoured nozzle for the HEG. Deutsche Forschungsanstalt fur Luft- und Raumfahrt, 1990.

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Book chapters on the topic "Wind tunnels – Design"

1

Brownlie, Len W. "Wind Tunnels: Design Considerations in Wind Tunnel Testing of Cyclists." In Biomechanical Principles and Applications in Sports. Springer International Publishing, 2019. http://dx.doi.org/10.1007/978-3-030-13467-9_4.

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Filgueiras, Ernesto, and Daniel Bacelar Pereira. "Physical and Virtual Wind Tunnels: Automobile Design Approach." In Advances in Ergonomics in Design. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-79760-7_92.

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Fujino, Yozo, Kichiro Kimura, and Hiroshi Tanaka. "Wind Tunnel Tests." In Wind Resistant Design of Bridges in Japan. Springer Japan, 2012. http://dx.doi.org/10.1007/978-4-431-54046-5_6.

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Kämpchen, M., H. Korsch, A. Dafnis, and H. G. Reimerdes. "Design, Qualification and Experimental Investigation on Flexible Wind Tunnel Wing Models." In Flow Modulation and Fluid—Structure Interaction at Airplane Wings. Springer Berlin Heidelberg, 2003. http://dx.doi.org/10.1007/978-3-540-44866-2_15.

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Kirchheck, Daniel, Dominik Saile, and Ali Gülhan. "Rocket Wake Flow Interaction Testing in the Hot Plume Testing Facility (HPTF) Cologne." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_9.

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Abstract Rocket wake flows were under investigation within the Collaborative Research Centre SFB/TRR40 since the year 2009. The current paper summarizes the work conducted during its third and final funding period from 2017 to 2020. During that phase, focus was laid on establishing a new test environment at the German Aerospace Center (DLR) Cologne in order to improve the similarity of experimental rocket wake flow–jet interaction testing by utilizing hydrogen–oxygen combustion implemented into the wind tunnel model. The new facility was characterized during tests with the rocket combustor model HOC1 in static environment. The tests were conducted under relevant operating conditions to demonstrate the design’s suitability. During the first wind tunnel tests, interaction of subsonic ambient flow at Mach 0.8 with a hot exhaust jet of approx. 920 K was compared to previously investigated cold plume interaction tests using pressurized air at ambient temperature. The comparison revealed significant differences in the dynamic response of the wake flow field on the different types of exhaust plume simulation.

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Hühne, Claus-Philipp, Peter Scholz, and Rolf Radespiel. "Aerodynamic Effects of Tip Tanks on a Swept Wing Wind-Tunnel Model." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2014. http://dx.doi.org/10.1007/978-3-319-03158-3_50.

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Streit, Thomas, Heiko Geyr von Schweppenburg, David Cruz, and Rafael Sanchez. "DLR Feasibility Study of HLFC Wing Designs for S1MA Wind Tunnel Test." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2021. http://dx.doi.org/10.1007/978-3-030-79561-0_23.

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Heryawan, Yudi, Hoon Cheol Park, Nam Seo Goo, Kwang Joon Yoon, and Yung Hwan Byun. "Structural Design, Manufacturing, and Wind Tunnel Test of a Small Expandable Wing." In Fracture and Strength of Solids VI. Trans Tech Publications Ltd., 2006. http://dx.doi.org/10.4028/0-87849-989-x.1157.

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Génin, Chloé, Dirk Schneider, and Ralf Stark. "Dual-Bell Nozzle Design." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_25.

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Abstract The dual-bell nozzle is an altitude adaptive nozzle concept that offers two operation modes. In the framework of the German Research Foundation Special Research Field SFB TRR40, the last twelve years have been dedicated to study the dual-bell nozzle characteristics, both experimentally and numerically. The obtained understanding on nozzle contour and inflection design, transition behavior and transition prediction enabled various follow-ups like a wind tunnel study on the dual-bell wake flow, a shock generator study on a film cooled wall inflection or, in higher scale, the hot firing test of a thrust chamber featuring a film cooled dual-bell nozzle. A parametrical system study revealed the influence of the nozzle geometry on the flow behavior and the resulting launcher performance increase.

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Zasso, Alberto, Paolo Schito, Carlo L. Bottasso, and Alessandro Croce. "Aero-Servo-Elastic Design of Wind Turbines: Numerical and Wind Tunnel Modeling Contribution." In Environmental Wind Engineering and Design of Wind Energy Structures. Springer Vienna, 2011. http://dx.doi.org/10.1007/978-3-7091-0953-3_4.

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Conference papers on the topic "Wind tunnels – Design"

1

Duncan, James. "Heat exchanger design considerations for transonic wind tunnels." In 20th AIAA Advanced Measurement and Ground Testing Technology Conference. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-2617.

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Nouri-Borujerdi, A., and M. Ziaei-Rad. "Numerical Solution of Transient Flow in Wind Tunnels." In ASME 7th Biennial Conference on Engineering Systems Design and Analysis. ASMEDC, 2004. http://dx.doi.org/10.1115/esda2004-58194.

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This paper deals with design and analysis of intermittent supersonic wind tunnels. System can be constructed by allowing air at atmospheric pressure to pass through a converging-diverging nozzle, a test section and a diffuser into a vacuum tank. The governing equations of compressible fluid flow have been solved numerically using flux vector splitting method to obtain running time under which it works at the design Mach number. The formulation has been tested on the theory of quasi one-dimensional compressible flow. The numerical results are in good agreement with the results of the theory.

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Matsuzaki, R. "Design of contoured nozzle for arc-heated wind tunnels." In 25th Plasmadynamics and Lasers Conference. American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-2593.

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Wang, Zhu, Jaehoon Han, and Ales Alajbegovic. "Nozzle Effects in Thermal Wind Tunnels." In ASME 2010 3rd Joint US-European Fluids Engineering Summer Meeting collocated with 8th International Conference on Nanochannels, Microchannels, and Minichannels. ASMEDC, 2010. http://dx.doi.org/10.1115/fedsm-icnmm2010-31171.

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Presented is an investigation of the wind-tunnel nozzle effects on the thermal performance within passenger vehicle underhood area. The Lattice-Boltzmann Equation (LBE) based flow solver is coupled with the system tool to solve for airflow and temperature distribution around the passenger vehicle in the wind tunnel. Several simulations with different nozzle sizes were performed. The simulation results are compared with airflow, temperature, and heat exchangers heat rejection measurements in the thermal wind tunnel. Good agreement is observed confirming that nozzle geometry dominates the airflo

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Beck, B. Terry, and Nelson A. Pratt. "A Simple Device for Wind Tunnel Performance Testing of Small Scale Powered Propellers." In ASME 2005 Fluids Engineering Division Summer Meeting. ASMEDC, 2005. http://dx.doi.org/10.1115/fedsm2005-77191.

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Propellers represent an interesting application of the principles of aerodynamics. The basic physics of propeller operation can be modeled as a rotating wing section using classical blade element analysis procedure, which can also include flows induced by the propeller motion itself. Performance testing of small-scale powered propellers in modest size educational wind tunnels could yield important verification of these analysis tools, and also provide valuable experimental insight into important aspects of propeller design for the engineering laboratory. To provide useful data, measurements of

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BECKWITH, I., F. J. CHEN, and M. MALIK. "Design and fabrication requirements for low-noise supersonic/hypersonic wind tunnels." In 26th Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 1988. http://dx.doi.org/10.2514/6.1988-143.

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Bruckmann, Tobias, Lars Mikelsons, Thorsten Brandt, Dieter Schramm, Andreas Pott, and Moustafa Abdel-Maksoud. "A Novel Tensed Mechanism for Simulation of Maneuvers in Wind Tunnels." In ASME 2009 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. ASMEDC, 2009. http://dx.doi.org/10.1115/detc2009-86718.

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Wind tunnels are a standard tool to evaluate the air flow properties of aerodynamical vehicles in model scale. This is widely used to optimize the design of aircrafts and aircraft components. Additionally, the hydrodynamic properties of marine components like ship hulls or propulsion systems can be predicted. It is desirable to guide the models along defined trajectories during the tests to vary the angle of attack. Parallel wire robots were successfully used to perform airplane maneuvers in wind tunnels due to their good aerodynamical and mechanical properties. Compared to aircraft design, ma

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Marino, Antonello, and Aldo Bonfiglioli. "Optimization of the Porosity Distribution in Transonic Wind Tunnel." In ASME 2012 Fluids Engineering Division Summer Meeting collocated with the ASME 2012 Heat Transfer Summer Conference and the ASME 2012 10th International Conference on Nanochannels, Microchannels, and Minichannels. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/fedsm2012-72487.

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During past years, to improve the quality of wind tunnel data in transonic configurations, researchers first designed new wind tunnel geometries (as porous and/or slotted wind tunnels), then developed more accurate correction laws giving acceptable results in certain conditions but absolutely not sufficient to satisfy the increasing aeronautical requirements. Recent studies showed that the quality of wind tunnel data can be improved by using test sections provided with variable streamwise porosity distributions instead of the typical uniform ones. Some authors identified this new concept of va

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Zheng, Ya-qing. "Feedback Linearization Control of a Wire-Driven Parallel Support System in Wind Tunnels." In Sixth International Conference on Intelligent Systems Design and Applications. IEEE, 2006. http://dx.doi.org/10.1109/isda.2006.27.

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Huang, Chih-Yung, Zih-Chen Lin, and Chen-Yu Hsiao. "Design and Fabrication of Micro-Supersonic Wind Tunnels for Microscale Shock Wave Analysis." In AIAA Scitech 2021 Forum. American Institute of Aeronautics and Astronautics, 2021. http://dx.doi.org/10.2514/6.2021-0833.

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Reports on the topic "Wind tunnels – Design"

1

Grossir, Guillaume. On the design of quiet hypersonic wind tunnels. Von Karman Institute for Fluid Dynamics, 2020. http://dx.doi.org/10.35294/tm57.

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This document presents a thorough literature review on the development of hypersonic quiet tunnels. The concept of boundary layer transition in high-speed flows is presented first. Its consequences on the free-stream turbulence levels in ground facilities are reviewed next, demonstrating that running boundary layers along the nozzle walls must remain laminar for quiet operation. The design key points that enable laminar boundary layers and hypersonic operation with low free-stream noise levels are then identified and discussed. The few quiet facilities currently operating through the world are

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2

Wagner, Matthew J., and Gary A. Dale. The Design and Testing of Pneumatic Systems for Measuring Low Pressures in Hypersonic Wind Tunnels. Defense Technical Information Center, 1985. http://dx.doi.org/10.21236/ada379715.

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Mayda, Edward A., C. P. van Dam, David D. Chao, and Dale E. Berg. Computational design and analysis of flatback airfoil wind tunnel experiment. Office of Scientific and Technical Information (OSTI), 2008. http://dx.doi.org/10.2172/961975.

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Lipinski, R. J., and R. P. Kensek. Conceptual design for an electron-beam heated hypersonic wind tunnel. Office of Scientific and Technical Information (OSTI), 1997. http://dx.doi.org/10.2172/522724.

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Marshall, R. D. Performance requirements and preliminary design of a boundary layer wind tunnel facility. National Bureau of Standards, 1985. http://dx.doi.org/10.6028/nbs.ir.85-3168.

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Brown, C. R. Preliminary Nozzle Design for use in a Small-Scale, High Mach Number Wind Tunnel. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1568032.

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SCHNEIDER, LARRY X. Conceptual Design of a 50--100 MW Electron Beam Accelerator System for the National Hypersonic Wind Tunnel Program. Office of Scientific and Technical Information (OSTI), 2000. http://dx.doi.org/10.2172/759452.

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Pitts, William M. Assessment of need for and design requirements of a wind tunnel facility to study fire effects of interest to DNA. National Institute of Standards and Technology, 1989. http://dx.doi.org/10.6028/nist.ir.89-4049.

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