Three-Dimensional Numerical Study of the Conical Nozzle Side Loads during Staging-Reference-Cited by-同舟云学术

Three-Dimensional Numerical Study of the Conical Nozzle Side Loads during Staging

Published:2016-09 Issue:5 Volume:29 Page:04016038
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Jia Ruyan¹,Jiang Zhenyu²,Xiang Min²,Zhang Weihua³

Affiliation:

1. Ph.D. Student, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China (corresponding author).

2. Associate Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China.

3. Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, Changsha 410073, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000629

Reference33 articles.

1. Alziary De Roquefort T. (2002). “Low frequency fluctuations in separated turbulent compressible flows.” Symp. on Advanced Fluid Tokyo.

2. ANSYS 14.0 [Computer software]. ANSYS Canonsburg PA.

3. Bowyer J. M. Kreiter G. W. and Petersen R. E. (1978). “An investigation of the side force that is sometimes observed in rocket motor start-up.” AIAA Paper 78-104514th Joint Propulsion Conf. AIAA Reston VA.

4. Cikanek H. A. (1987). “Characteristics of space shuttle main engine failures.” AIAA Paper 87-193923rd Joint Propulsion Conf. AIAA Reston VA.

5. Delayed detached eddy simulation of the end-effect regime and side-loads in an overexpanded nozzle flow

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