Modeling of an Exhaust Gas Cooler in a High-Altitude Test Facility of Large-Area Ratio Rocket Engines-Reference-Cited by-同舟云学术

Modeling of an Exhaust Gas Cooler in a High-Altitude Test Facility of Large-Area Ratio Rocket Engines

Published:2015-01 Issue:1 Volume:28 Page:04014049
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Rajagopal Manikanda¹,Rajamanohar D.²

Affiliation:

1. Purdue School of Engineering and Technology, Indiana Univ.-Purdue Univ. Indianapolis, IN; formerly, Ph.D. Scholar, Dept. of Mechanical Engineering, Indian Institute of Technology Madras, Chennai, India (corresponding author).

2. Deputy General Manager, Liquid Propulsion Systems Center, Indian Space Research Organization (ISRO), Mahendragiri, India.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000378

Reference13 articles.

1. Evaluation of the performance of supersonic exhaust diffuser using scaled down models

2. Droplet evaporation with reference to the effectiveness of water-mist cooling

3. Characteristic features of evaporative cooling of droplets in high-temperature flows

4. An analysis of the d2-law departure during droplet evaporation in microgravity

5. Evaporative cooling of water in a mechanical draft cooling tower

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