Influence of Fuel Boiling Point on Discharge Characteristics of Superheated Hydrocarbon Liquid Jets

Author:

Yoo Young Joon,Lee Hyung JuORCID,Choi Hojin,Jeong Byunghun,Han Jeongsik

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Reference27 articles.

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2. National Research Council (1998) Review and evaluation of the air force hypersonic technology program. National Academy Press, Washington, DC, pp 5–17

3. Cooper M, Shepherd JE (2002) Thermal and catalytic cracking of JP-10 for pulse detonation engine applications, GALCIT Report FM 2002.002, Caltech

4. Gasner JA, Foster RC, Fujimura C (1992) Evaluation of thermal management for a Mach 5.5 hypersonic vehicle, AIAA 92-3721

5. Sobel DR, Spadaccini LJ (1997) Hydrocarbon fuel cooling technologies for advanced propulsion. ASME J Eng Gas Turbines Power 119:344–351

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