International Journal of

ADVANCED AND APPLIED SCIENCES

EISSN: 2313-3724, Print ISSN: 2313-626X

Frequency: 12

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 Volume 9, Issue 12 (December 2022), Pages: 98-107

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 Original Research Paper

 Wave drag coefficient of nonaxisymmetric irregular-shaped bodies

 Author(s): Sabina Serdarevic-Kadic *

 Affiliation(s):

 Mechanical Engineering Faculty, University of Sarajevo, Sarajevo, Bosnia and Herzegovina

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 * Corresponding Author. 

  Corresponding author's ORCID profile: https://orcid.org/0000-0003-3163-501X

 Digital Object Identifier: 

 https://doi.org/10.21833/ijaas.2022.12.013

 Abstract:

At high speeds, transonic and supersonic, the wave drag coefficient is a significant part of drag coefficients and it depends on the front surface shape and flow velocity. Drag, wave drag, drag coefficient, and wave drag coefficient for four bodies with the same width, height and length, and different shapes are estimated by CFD (ANSYS Fluent). For different front surface curvatures, at high flow velocity, pressure distribution on the front surface of the body, and flow field as a contour of Mach number are analyzed. The influence of front surface curvature on detached shock wave distance is determined.

 © 2022 The Authors. Published by IASE.

 This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

 Keywords: Wave drag coefficient, Flow field, Pressure, Mach number

 Article History: Received 28 April 2022, Received in revised form 20 July 2022, Accepted 2 September 2022

 Acknowledgment 

No Acknowledgment.

 Compliance with ethical standards

 Conflict of interest: The author(s) declared no potential conflicts of interest with respect to the research, authorship, and/or publication of this article.

 Citation:

 Serdarevic-Kadic S (2022). Wave drag coefficient of nonaxisymmetric irregular-shaped bodies. International Journal of Advanced and Applied Sciences, 9(12): 98-107

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 Figures

 Fig. 1 Fig. 2 Fig. 3 Fig. 4 Fig. 5 Fig. 6 Fig. 7 Fig. 8 Fig. 9 

 Tables

 Table 1 Table 2

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