THERMAL SCIENCE

International Scientific Journal

Songjian Hu

,

Shuaibin Qu

,

Zhimeng Zheng

,

Pengyu Zhu

,

Chenghao Zou

,

Yiqing Li

INVESTIGATION OF AERODYNAMICS EDUCATION BASED ON THE WAVERIDER PARAMETERIZED DESIGN PROCEDURE

ABSTRACT
This paper describes the development and coding of a design tool for waverider parameterization based on the Taylor-Maccoll equation and streamline tracing method. This tool, intended for undergraduates studying in the field of aerody-namics, illustrates the relationship among various parameters in terms of their effect on the aerodynamic performance of waverider models with the same freestream Mach number. The design procedure is evaluated and validated for multiple shock wave profiles and freestream Mach numbers, and is found to be in good agreement with the CFD results. For undergraduates studying aeronautical engineering, the suggested design tool offers an intuitive image of waverider cre-ation and a clear picture of the guiding principles of waveriders. By imposing a set of design criteria, the tool also gives students enough freedom to arrive at their own waverider shape.
KEYWORDS
waverider, aerodynamic, parameterize design
PAPER SUBMITTED: 2022-03-11
PAPER REVISED: 2023-01-12
PAPER ACCEPTED: 2023-01-13
PUBLISHED ONLINE: 2023-02-11
DOI REFERENCE: https://doi.org/10.2298/TSCI220311032H
CITATION EXPORT: view in browser or download as text file
THERMAL SCIENCE YEAR 2023, VOLUME 27, ISSUE Issue 2, PAGES [1393 - 1404]
REFERENCES
  1. Yu, K., et al., Inverse Design Methodology of Cone-Derived Waverider Based on Pre-Defined Shock Wave Under Strong Geometric Constraints, Acta Astronautica, 159 (2019), June, pp. 527-539
  2. Li, Y., et al. Dual Waverider to Integrate External and Internal Flows, J. of Aircraft, 57 (2020), 3, pp. 428-439
  3. Bykerk, T., et al., Low Speed Lateral-Directional Aerodynamic and Static Stability Analysis of a Hyper-sonic Waverider, Aerosp. Sci. Technol., 98 (2020), 105709
  4. Zhao, Z. T., et al., An Overview of Research on Wide-Speed Range Waverider Configuration, Prog. Aerosp. Sci., 113 (2020), 100606
  5. Li, S. B., et al., Design and Investigation of Equal Cone-Variable Mach Number Waverider in Hyper-sonic Flow, Aerosp. Sci. Technol., 96 (2020), 105540
  6. Billig, F. S., Kothari, A. P., Streamline Tracing: Technique for Designing Hypersonic Vehicles, J. Pro-puls. Power., 16 (2000), 3, pp. 465-471
  7. Anderson, J. D., Jr, Fundamentals of Aerodynamics, McGraw-Hill Education,New York, USA, 2017
  8. Bertin, J., John, M. L., Smith, Aerodynamics for Engineers, Prentice-Hall, Inc., Englewood Cliffs, Upper Saddle River, N. J., USA, 1979
  9. Munson, B. R., et al., Fundamentals of Fluid Mechanics, 6th ed., John Wiley & Sons Inc, New York, USA, 2009
  10. Ding, F., et al., An Overview of Waverider Design Concept in Airframe/Inlet Integration Methodology for Air-Breathing Hypersonic Vehicles, Acta Astronaut., 152 (2018), Nov., pp. 639-656
  11. Nonweiler, T. R. F., Aerodynamic Problems of Manned Space Vehicle, J. Roy. Aeronaut. Soc., 63 (1959), pp. 521-528
  12. Rasmussen, M., Waverider Configurations Derived from Inclined Circular and Elliptic Cones, J. Spacecr. Rockets., 17 (1980), 6, pp. 537-545
  13. Sobieczky, H., et al., Hypersonic Waverider Design from Given Shock Waves, Proceedings, Interna-tional Hypersonic Waverider Symposium, University of Maryland, College Park, Md., USA, 1990
  14. Jones, K. D., et al., Waverider Design for Generalized Shock Geometries, J. Spacecr. Rockets, 32 (1993), 6, pp. 957-963
  15. Ding, F., et al. Novel Inlet-Airframe Integration Methodology for Hypersonic Waverider Vehicles, Acta Astronautica, 111 (2015), June-July, pp. 178-197
  16. Center, K. B., et al., Interactive Design of Hypersonic Waverider Geometries, Proceedings, 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference, Honolulu, Hi., USA, 1991
  17. Hu, S. Y., et al., Combined-Wedge Waverider for Airframe-Propulsion Integration, AIAA Journal, 56 (2018), 8, pp. 3348-3352
  18. Sobieczky, H., et al., High Speed Flow Design Using Osculating Axisymmetric Flows, Proceedings, 3rd Pacific International Conference on Aerospace Science and Technology, Xian, China, 1997, pp. 182-187
  19. Jones, J. G., et al., A Method for Designing Lifting Configurations for High Supersonic Speeds, Using Axisymmetric Flow Fields, Ingenieur Archiv, 37 (1968), 1, pp. 56-72
  20. Rasmussen, M., Brandes-Dunkam, B., Hypersonic Waveriders Generated from Power-Law Shocks, Proceedings, International Aerospace Planes and Hypersonics Technologies, Chattanooga, Tenn., USA, 1995
  21. He, X. Z., et al., Design and Analysis Osculating General Curved Cone Waverider, Aircraft Engineering and Aerospace Technology, 89 (2017), 6, pp. 797-83
  22. Rodi, P., The Osculating Flowfield Method of Waverider Geometry Generation, Proceedings, 43rd AI-AA Aerospace Sciences Meeting and Exhibit, Reno, Nev., USA, 2005
  23. Rodi, P., Geometrical Relationships for Osculating Cones and Osculating Flowfield Waveriders, Pro-ceedings, 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Fla., USA, 2011
  24. Chen, L. L., et al., Waverider Configuration Design with Variable Shock Angle, IEEEAccess, 7 (2019), Mar., pp. 42081-42093
  25. Chen, L. L., et al., A Novel Approach for Design and Analysis of Volume-Improved Osculating-Cone Waveriders, Acta Astronautica, 161 (2019), Aug., pp. 430-445
  26. Liu, J., et al., Novel Approach for Designing a Hypersonic Gliding-Cruising Dual Waverider Vehicle, Acta Astronautica, 102 (2014), Sept., pp. 81-88
  27. Li, S. B., et al., Design and Investigation on Variable Mach Number Waverider for a WideSpeed Range, Aerospace Science and Technology, 76 (2018), May, pp. 291-302
  28. Zhao, Z. T., et al., Variable Mach Number Design Approach for a Parallel Waverider with a WideSpeed Range Based on the Osculating Cone Theory, Acta Astronautica, 147 (2018), June, pp. 163-174
PDF VERSION [DOWNLOAD]
Investigation of aerodynamics education based on the waverider parameterized design procedure

© 2024 Society of Thermal Engineers of Serbia. Published by the Vinča Institute of Nuclear Sciences, National Institute of the Republic of Serbia, Belgrade, Serbia. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution-NonCommercial-NoDerivs 4.0 International licence