Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule

Zhang Zhang; Liwu Wang; Wei Huang; Jiangli Lei; Rui Zhao

doi:10.1007/978-981-13-3305-7_19

Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule

Zhang Zhang^*, Liwu Wang, Wei Huang, Jiangli Lei, Rui Zhao

^*Corresponding author for this work

School of Aerospace Engineering

China Aerospace Science and Technology Corporation

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

Abstract

Aerodynamic performance and surface flow of reentry capsule are important for altitude static pressure tapping location design and pressure coefficient calibration. A capsule CFD model is presented and aerodynamic performance in different Mach number, angle-of-attack (AOA) and angle-of-side-slip (AOSS) is investigated in this paper. Based on statistics principle of minimum variance and deviation, location optimization design of altitude static pressure tapping is also conducted in this paper. The result shows numerical accuracy of aerodynamic performance is validated through comparison with wind tunnel test results. Aerodynamic performance of the reentry capsule is in a steady level from −30° to 30° AOA and −10° to 10° AOSS. High absolute value of positive and negative AOA & AOSS can significantly induce deterioration of capsule aerodynamic performance. According to statistics principle of minimum variance and deviation, three appropriate tapping points are obtained. With pressure coefficient histogram analysis, ideal altitude static pressure tapping location is selected.

Original language	English
Title of host publication	The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018
Editors	Xinguo Zhang
Publisher	Springer Verlag
Pages	236-243
Number of pages	8
ISBN (Print)	9789811333040
DOIs	https://doi.org/10.1007/978-981-13-3305-7_19
Publication status	Published - 2019
Event	Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018 - Chengdu, China Duration: 16 Oct 2018 → 18 Oct 2018

Publication series

Name	Lecture Notes in Electrical Engineering
Volume	459
ISSN (Print)	1876-1100
ISSN (Electronic)	1876-1119

Conference

Conference	Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018
Country/Territory	China
City	Chengdu
Period	16/10/18 → 18/10/18

Keywords

Aerodynamic performance
Altitude static pressure tapping
Capsule
Numerical simulation
Optimization design

Access to Document

10.1007/978-981-13-3305-7_19

Cite this

Zhang, Z., Wang, L., Huang, W., Lei, J., & Zhao, R. (2019). Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule. In X. Zhang (Ed.), The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018 (pp. 236-243). (Lecture Notes in Electrical Engineering; Vol. 459). Springer Verlag. https://doi.org/10.1007/978-981-13-3305-7_19

@inproceedings{e961b374cb4740ddb809cf5fbe23544e,

title = "Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule",

abstract = "Aerodynamic performance and surface flow of reentry capsule are important for altitude static pressure tapping location design and pressure coefficient calibration. A capsule CFD model is presented and aerodynamic performance in different Mach number, angle-of-attack (AOA) and angle-of-side-slip (AOSS) is investigated in this paper. Based on statistics principle of minimum variance and deviation, location optimization design of altitude static pressure tapping is also conducted in this paper. The result shows numerical accuracy of aerodynamic performance is validated through comparison with wind tunnel test results. Aerodynamic performance of the reentry capsule is in a steady level from −30° to 30° AOA and −10° to 10° AOSS. High absolute value of positive and negative AOA & AOSS can significantly induce deterioration of capsule aerodynamic performance. According to statistics principle of minimum variance and deviation, three appropriate tapping points are obtained. With pressure coefficient histogram analysis, ideal altitude static pressure tapping location is selected.",

keywords = "Aerodynamic performance, Altitude static pressure tapping, Capsule, Numerical simulation, Optimization design",

author = "Zhang Zhang and Liwu Wang and Wei Huang and Jiangli Lei and Rui Zhao",

note = "Publisher Copyright: {\textcopyright} 2019, Springer Nature Singapore Pte Ltd.; Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018 ; Conference date: 16-10-2018 Through 18-10-2018",

year = "2019",

doi = "10.1007/978-981-13-3305-7_19",

language = "English",

isbn = "9789811333040",

series = "Lecture Notes in Electrical Engineering",

publisher = "Springer Verlag",

pages = "236--243",

editor = "Xinguo Zhang",

booktitle = "The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018",

address = "Germany",

}

Zhang, Z, Wang, L, Huang, W, Lei, J & Zhao, R 2019, Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule. in X Zhang (ed.), The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018. Lecture Notes in Electrical Engineering, vol. 459, Springer Verlag, pp. 236-243, Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018, Chengdu, China, 16/10/18. https://doi.org/10.1007/978-981-13-3305-7_19

Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule. / Zhang, Zhang; Wang, Liwu; Huang, Wei et al.
The Proceedings of the Asia-Pacific International Symposium on Aerospace Technology, APISAT 2018. ed. / Xinguo Zhang. Springer Verlag, 2019. p. 236-243 (Lecture Notes in Electrical Engineering; Vol. 459).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule

AU - Zhang, Zhang

AU - Wang, Liwu

AU - Huang, Wei

AU - Lei, Jiangli

AU - Zhao, Rui

PY - 2019

Y1 - 2019

N2 - Aerodynamic performance and surface flow of reentry capsule are important for altitude static pressure tapping location design and pressure coefficient calibration. A capsule CFD model is presented and aerodynamic performance in different Mach number, angle-of-attack (AOA) and angle-of-side-slip (AOSS) is investigated in this paper. Based on statistics principle of minimum variance and deviation, location optimization design of altitude static pressure tapping is also conducted in this paper. The result shows numerical accuracy of aerodynamic performance is validated through comparison with wind tunnel test results. Aerodynamic performance of the reentry capsule is in a steady level from −30° to 30° AOA and −10° to 10° AOSS. High absolute value of positive and negative AOA & AOSS can significantly induce deterioration of capsule aerodynamic performance. According to statistics principle of minimum variance and deviation, three appropriate tapping points are obtained. With pressure coefficient histogram analysis, ideal altitude static pressure tapping location is selected.

AB - Aerodynamic performance and surface flow of reentry capsule are important for altitude static pressure tapping location design and pressure coefficient calibration. A capsule CFD model is presented and aerodynamic performance in different Mach number, angle-of-attack (AOA) and angle-of-side-slip (AOSS) is investigated in this paper. Based on statistics principle of minimum variance and deviation, location optimization design of altitude static pressure tapping is also conducted in this paper. The result shows numerical accuracy of aerodynamic performance is validated through comparison with wind tunnel test results. Aerodynamic performance of the reentry capsule is in a steady level from −30° to 30° AOA and −10° to 10° AOSS. High absolute value of positive and negative AOA & AOSS can significantly induce deterioration of capsule aerodynamic performance. According to statistics principle of minimum variance and deviation, three appropriate tapping points are obtained. With pressure coefficient histogram analysis, ideal altitude static pressure tapping location is selected.

KW - Aerodynamic performance

KW - Altitude static pressure tapping

KW - Capsule

KW - Numerical simulation

KW - Optimization design

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ER -

Numerical Investigation on Altitude Static Pressure Tapping Location Design of a Reentry Capsule

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