Experimental Study on RP-3 Aviation Fuel Tank Using Oxygen-Consuming Inerting Technology

Author:

Peng Xiaotian1ORCID,Wang Hongming2,Huang Long3,Peng Hao4,Wang Yangyang5,Feng Shiyu6

Affiliation:

1. Ph.D. Candidate, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Yudao St., Nanjing 210016, China. ORCID: .

2. Professor, Jiangsu Maritime Institute, No. 309 Gezhi Rd., Nanjing 211170, China.

3. Lecturer, College of Marine Electrical and Intelligent Engineering, Jiangsu Maritime Institute, No. 309 Gezhi Rd., Nanjing 211170, China.

4. Associate Professor, Merchant Marine College, Shanghai Maritime Univ., No. 1550 Harbour Ave., Shanghai 201306, China.

5. Engineer, Aviation Key Laboratory of Science and Technology on Aero Electromechanical System Integration, Nanjing Engineering Institute of Aircraft Systems, No. 33 Shuige Rd., Nanjing 211106, China.

6. Associate Professor, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, No. 29 Yudao St., Nanjing 210016, China (corresponding author).

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Reference17 articles.

1. Anderson C.-L. 1978. “Test and evaluation of Halon 1301 and nitrogen inerting against 23mm HEI projectiles.” Accessed May 3 1978. https://www.fire.tc.faa.gov/pdf/systems/AFFDL_TR_78_66.pdf.

2. Wall Heat Flux Measurements for a Kerosene-Fueled Supersonic Combustor

3. Method and System for Making a Fuel-tank Inert without an Inert Gas

4. Main Wheel Prerotation and Ground Taxi Driven by Electric Taxi System

5. Combustion Characteristics of Paraffin-Polyethylene Blends Fuel for Solid Fuel Ramjet

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