Conceptual Aerodynamic Design of Pintle Nozzle for Variable-Thrust Propulsion

Comprehensive theoretical studies have been carried out for the geometry optimization of a pintle nozzle for variable-thrust propulsion. We designed the pintle such that, at the final pintle position, the integrated shape facilitates the scaled-down version of the shockless main nozzle. Numerical st...

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Bibliographic Details

Published in:	International journal of aeronautical and space sciences Vol. 21; no. 1; pp. 1 - 14
Main Authors:	Saravanan, Vignesh, Ko, Jeongwoo, Lee, Soogab, Murugan, Nijanthan, Kumar, V. R. Sanal
Format:	Journal Article
Language:	English
Published:	Seoul The Korean Society for Aeronautical & Space Sciences (KSAS) 01-03-2020 한국항공우주학회
Subjects:	Aerospace Technology and Astronautics Engineering Fluid- and Aerodynamics Original Paper 항공우주공학 Pintle nozzle Aerodynamic design Nozzle performance Quasi-dynamic analysis
Online Access:	Get full text
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