Relevant bibliographies by topics / Delta wing airplanes

Contents

  1. Journal articles
  2. Dissertations / Theses
  3. Books
  4. Conference papers

Academic literature on the topic 'Delta wing airplanes'

Author: Grafiati
Published: 4 June 2021
Last updated: 27 July 2025

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Journal articles on the topic "Delta wing airplanes"

1

Mochizuki, Saya, and Gouji Yamada. "Aerodynamic characteristics and flow field of delta wings with the canard." MATEC Web of Conferences 145 (2018): 03010. http://dx.doi.org/10.1051/matecconf/201814503010.

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Now, many kinds of explorations for outer planets have been proposed around the world. Among them Mars attracts much attention for future exploration. Orbiters and landers have been used for Mars exploration. Recently as a new exploration method, the usage of an airplane has been seriously considered and there are some development projects for Mars airplane. However, the airplane flying on the Earth atmosphere cannot fly on the Mars atmosphere, because atmospheric conditions are much different each other. Therefore, we focused on the usage of the airplane with unfolding wings for Mars explorat
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2

Deng, Xiaogang, Meiliang Mao, Guohua Tu, Hanxin Zhang, and Yifeng Zhang. "High-Order and High Accurate CFD Methods and Their Applications for Complex Grid Problems." Communications in Computational Physics 11, no. 4 (2012): 1081–102. http://dx.doi.org/10.4208/cicp.100510.150511s.

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AbstractThe purpose of this article is to summarize our recent progress in high-order and high accurate CFD methods for flow problems with complex grids as well as to discuss the engineering prospects in using these methods. Despite the rapid development of high-order algorithms in CFD, the applications of high-order and high accurate methods on complex configurations are still limited. One of the main reasons which hinder the widely applications of these methods is the complexity of grids. Many aspects which can be neglected for low-order schemes must be treated carefully for high-order ones
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3

Alizadeh, Asad, and Anas Abid Mattie. "Numerical simulation of the formation of vortices around rigid cylinders inside a channel using Immersed Interface method." Mechanics 26, no. 1 (2020): 18–24. http://dx.doi.org/10.5755/j01.mech.26.1.23186.

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The numerical simulation of the flow of fluid through one or a set of objects that causes the flow to separate from the surface of them has been the subject of interest by researchers over the past few decades. One of the most important types of these objects is those with a square cross section which have important and diverse applications in different industries. One of the practical applications of these types of streams is flow around chimneys, high-rise buildings, naval structures, suspended bridges, airplane wings, ship propellers and ducts. In this research, the immersed interface metho
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4

Singh, S. Rajat, and Y. D. Dwivedi. "IMPLEMENTATION OF TRANSONIC AREA RULE AND SWEPT BACK DELTA WING DESIGN ON AN AIRCRAFT." Graduate Research in Engineering and Technology, January 2022, 20–25. http://dx.doi.org/10.47893/gret.2022.1050.

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The transonic area rule was first implemented in the 1950s. It is an important concept related to the drag on an aircraft or other body in transonic and supersonic flight which states that two airplanes with the same longitudinal cross-sectional area distribution have the same wave drag, independent of how the area is distributed laterally. A swept back delta wing increases the critical Mach number of the wing and performs well at low speeds, as a result of unique swirling vortices that form on the upper surface of the wing. BOOM Supersonic plans to bring back Supersonic Commercial aircrafts b
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Chang, Min, Xiaoyu Feng, Yang Zhang, Xu Zhang, and Junqiang Bai. "Flow analysis on the ventral gap of a paper airplane." Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science, August 5, 2020, 095440622094607. http://dx.doi.org/10.1177/0954406220946076.

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It is a challenging work to design micro aerial vehicle with great aerodynamic performance because the tiny wingspan at low-Reynolds-number cannot provide lift efficiently. The aerodynamic configuration of a classic delta-wing paper airplane is investigated in the present work with numerical method to discover its potential for micro aerial vehicle designs. Furthermore, the effect of the ventral gap on the aerodynamic characteristics of the paper airplane is investigated herein. The stall angles of attack reach 37.5° and 40°, respectively, for ventral opened configuration and the closed one, a
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Dissertations / Theses on the topic "Delta wing airplanes"

1

Worley, John C. Ahmed Anwar. "Yaw-roll coupled oscillations of a slender delta wing." Auburn, Ala, 2008. http://repo.lib.auburn.edu/EtdRoot/2008/SUMMER/Aerospace_Engineering/Thesis/Worley_John_37.pdf.

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2

Hubner, James Paul. "An investigation of quasiperiodic structures in the vortical flow over Delta wing configuration." Diss., Georgia Institute of Technology, 1995. http://hdl.handle.net/1853/12243.

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3

Sung, Bongzoo. "Analysis of the vortical flow around a 60 degree delta wing with vortex flap." Diss., Virginia Polytechnic Institute and State University, 1985. http://hdl.handle.net/10919/49932.

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Subsonic wind tunnel investigations were conducted on a 60° swept, flat plate, delta wing with a leading edge vortex flap. The pressure distributions were measured over a range of angles of attack starting from zero to 40° in 5° interval and flap deflection angles from zero to 45° with 5° increments at a Reynolds number of about 2.14 x 10‘ based on the root chord. The flow visualization experiments were performed from zero degree to the stall angle, with ten different flap deflection angles at the same Reynolds number. The mean flow field was measured at angles of attack l0° and 15° with the f
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4

Thompson, Brad R. "Experimental investigation on the self-induction theory of vortex breakdown and new observations in the transient development of a delta wing leading edge vortex /." Thesis, Connect to this title online; UW restricted, 2007. http://hdl.handle.net/1773/7142.

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5

Cetek, Cem. "Aircraft control with nonlinear indicial response model." Ohio : Ohio University, 1999. http://www.ohiolink.edu/etd/view.cgi?ohiou1175888353.

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6

Srigrarom, Sutthiphong. "On the formation of vortex breakdown over delta wings /." Thesis, Connect to this title online; UW restricted, 2001. http://hdl.handle.net/1773/10004.

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7

Yavuz, Mehmet Metin. "Origin and control of the flow structure and topology on delta wings /." Diss., 2006. http://gateway.proquest.com/openurl?url_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:dissertation&res_dat=xri:pqdiss&rft_dat=xri:pqdiss:3203830.

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Books on the topic "Delta wing airplanes"

1

Leonard, Roberts, and United States. National Aeronautics and Space Administration., eds. Controlled vortical flow on delta wings through unsteady leading edge blowing. Stanford University, Dept. of Aeronautics and Astronautics, Joint Institute for Aeronautics and Acoustics, 1990.

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2

Wood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. Langley Research Center, 1987.

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3

B, Watson Carolyn, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Study of lee-side flows over conically cambered delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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4

A, Tavella D., Roberts Leonard, and United States. National Aeronautics and Space Administration., eds. Numerical study of delta wing leading edge blowing. Joint Institute for Aeronautics and Acoustics, 1988.

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5

Wood, Richard M. Study of lee-side flows over conically cambered delta wings at supersonic speeds. National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

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6

T, Batina John, and Langley Research Center, eds. Conical Euler simulation and active suppression of delta wing rocking motion. National Aeronautics and Space Administration, Langley Research Center, 1990.

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7

Center, Ames Research, ed. An aerodynamic model for one and two degree of freedom wing rock of slender delta wings. National Aeronautics and Space Administration, Ames Research Center, 1993.

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8

D, Hoffler Keith, and Langley Research Center, eds. A low speed wind tunnel study of vortex interaction control techniques on a chine-forebody/delta-wing configuration. National Aeronautics and Space Administration, Langley Research Center, 1992.

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9

United States. National Aeronautics and Space Administration., ed. Lift augmentation on a delta wing via leading edge fences and the Gurney flap. National Aeronautics and Space Administration, 1992.

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10

F, Sheta Essam, Massey Steven James, and United States. National Aeronautics and Space Administration., eds. Twin tail/Delta wing configuration buffet due to unsteady vortex breakdown flow. National Aeronautics and Space Administration, 1997.

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Conference papers on the topic "Delta wing airplanes"

1

Rea, Francesco, Francesco Amoroso, Rosario Pecora, and Markus Kintscher. "Design of an Adaptive Twist Trailing Edge for Large Commercial Aircraft Applications." In ASME 2018 Conference on Smart Materials, Adaptive Structures and Intelligent Systems. American Society of Mechanical Engineers, 2018. http://dx.doi.org/10.1115/smasis2018-7939.

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Researchers and engineers design modern aircraft wings to reach high levels of efficiency with the main outcome of weight saving and airplane lift-to-drag ratio increasing. Future commercial aircraft need to be mission-adaptive to improve their operational efficiency. Twistable trailing edge could be used to improve aircraft performances during climb and off-design cruise conditions in response to variations in speed, altitude, air temperature, and other flight parameters. Indeed, “continuous” span-wise twist of the wing trailing edge could provide significant reduction of the wing root bendin
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Chana, William. "World's first delta wing airplane Convair/Air Force XF-92A." In 2000 World Aviation Conference. American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-5515.

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3

Chana, William F. "World's First Delta Wing Airplane Convair/Air Force XF-92A." In World Aviation Congress & Exposition. SAE International, 2000. http://dx.doi.org/10.4271/2000-01-5515.

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4

Wen, Amin, Jianghua Zheng, Chen Mu, Jun Lin, and Peixian Li. "Application of delta-wing airplane remote sensing system with dual-camera in mapping vegetation fraction." In 2015 23rd International Conference on Geoinformatics. IEEE, 2015. http://dx.doi.org/10.1109/geoinformatics.2015.7378596.

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