Turbofan design options for mini UAV's-Reference-Cited by-同舟云学术

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Turbofan design options for mini UAV's

Published:2001-07-08 Issue: Volume: Page:
ISSN:
Container-title:37th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Rodgers C.¹

Affiliation:

1. ITC, San Diego, CA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2001-3969

Reference15 articles.

1. Aviation Week, "Subsonic Cruise Missile Engine Needed",June 281982,pg 201.

2. Cruzen.G.S. "Expendable Gas Turbine TechnologyAdvances"ACARD CP526,1994.

3. Epstein,A.K,etal,2000. "Shirtbutton-Sized Gas Turbines: TheEngineering ChallengesofMicro High Speed RotatingMachinery".ISROMAC-8 2000.

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1. Numerical and Experimental Investigations on Performance Optimization of a Microturbojet Engine Combustor;International Journal of Aerospace Engineering;2021-06-21

2. Effect of Variable Inlet Guide Vanes (VIGV) on a Small Gas Turbine Engine;AIAA Scitech 2021 Forum;2021-01-04

3. Development and Testing of a Fuzzy Logic Controller for a Small Turbojet Engine;54th AIAA Aerospace Sciences Meeting;2016-01-02

4. Turbofan multiobjective‐multipoint optimization for UAV/UCAV applications;Aircraft Engineering and Aerospace Technology;2013-08-30

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