Preliminary Estimation of Engine Gas-Flow-Path Size and Weight-Reference-Cited by-同舟云学术

Preliminary Estimation of Engine Gas-Flow-Path Size and Weight

Published:1998-03 Issue:2 Volume:14 Page:208-214
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Sanghi Vivek¹,Kumar S. Kishore¹,Sundararajan V.¹,Sane S. K.²

Affiliation:

1. Gas Turbine Research Establishment, Bangalore 560 093, India

2. Indian Institute of Technology, Bombay 400 076, India

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5269

Reference6 articles.

1. 1Sanghi, V. “Computer Aided Conceptual Design of Propulsion System for Combat Aircraft,” Ph.D. Dissertation, Indian Inst. of Technology, Bombay,India, 1996.

2. AIAA Education Series;Mattingly J. D.,1987

Cited by 12 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Comprehensive Flow Path Design Method for the Adaptive Cycle Engine Considering the Coupling Relation of Multiple Components;Journal of Engineering for Gas Turbines and Power;2024-04-04

2. A Preliminary Flow Path Design Tool for Advanced Aero-Engine;Lecture Notes in Electrical Engineering;2024

3. Gas Turbine/Solid Oxide Fuel Cell Hybrids for Aircraft Propulsion and Power;Journal of Propulsion and Power;2021-05

4. Influence of Flow Path Configuration on the Performance of Hybrid Turbine - Solid Oxide Fuel Cell Systems for Aircraft Propulsion and Power;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

5. Engine-integrated solid oxide fuel cells for efficient electrical power generation on aircraft;Journal of Power Sources;2015-06