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Combustion characteristics of swirl coaxial injectors at kerosene-rich conditions

  • Published:2013-04 Issue: Volume:106 Page:639-645
  • ISSN:0016-2361
  • Container-title:Fuel
  • language:en
  • Short-container-title:Fuel

Author:

Lim Byung-Jik,Seo Seonghyeon,Kim Munki,Ahn Kyubok,Kim Jong-Gyu,Choi Hwan-Seok

Publisher

Elsevier BV

Subject

Organic Chemistry,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering

Reference17 articles.

1. Zehetner HC. Liquid propellant gas generators. NASA SP-8081; 1972.

2. Harrje DT, Reardon FH, editors. Liquid propellant rocket combustion instability. Am psychol 1972.

3. Dennis Jr. HJ, Sanders T. NASA Fastrac engine gas generator component test program and results. In: 36th AIAA/ASME/SAE/ASEE joint propulsion conference. AIAA 2000-3401, Huntsville, Alabama; 2000.

4. Nesman TE, Dennis J. Fastrac gas generator testing. In: Tenth thermal and fluids analysis workshop. springer, September 13-17; 1999.

5. Mah CS. Evaluating the operational limits of a gas generator. In: 37th AIAA/ASME/SAE/ASEE joint propulsion conference. AIAA 2001–3990, Salt Lake City, UT; 2001.
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