Composite Cycle Engine Concept with Hectopressure Ratio
Author:
Affiliation:
1. Bauhaus Luftfahrt e.V., 85521 Munich, Germany
2. MTU Aero Engines AG, 80995 Munich, Germany
3. GKN Aerospace Sweden, SE-46181 Trollhättan, Sweden
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/10.2514/1.B35976
Reference32 articles.
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2. BradleyM. K.DroneyC. K. “Subsonic Ultra Green Aircraft Research Phase II: N+4 Advanced Concept Development,” NASA Rept. CR-2012-217556, May 2012.
3. LEMCOTEC: Improving the Core-Engine Thermal Efficiency
4. Advances in Gas Turbine Technology
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