Comparative Evaluation on the Deriving Method of the Heat Transfer Coefficient of the C-D Nozzle

Author:

Noh Tae Won,Roh Tae-Seong,Lee Hyoung Jin,Lee Hyunseob,Yoo Phil Hoon

Funder

LIG Nex1

Publisher

The Korean Society of Propulsion Engineers

Subject

General Medicine

Reference16 articles.

1. Bennett, C.O. and Myers, J.E., “Momentum, Heat, and Mass Transfer,“3rd edition, McGRAW-HILL, New York, N.Y., U.S.A, 1983.

2. A method of correlating forced convection heat-transfer data and a comparison with fluid friction

3. Bartz, D.R., “A simple equation for rapid estimation of rocket nozzle convective heat transfer coefficients,“ Jet Propulsion, Vol. 27, No. 1, pp. 49-51, 1957.

4. Turbulent Boundary-Layer Heat Transfer from Rapidly Accelerating Flow of Rocket Combustion Gases and of Heated Air

5. Betti, “Flow Field and Heat Transfer Analysis of Oxygen/Methane Liquid Rocket Engine Thrust Chambers,“ Ph.D. Thesis, Department of Mechanical and Aerospace Engineering, Sapienza University of Rome, Rome, Italy, 2012.

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