Exergy-Based Performance Assessment of the NASA Common Research Model

Author:

Arntz Aurélien1,Hue David1

Affiliation:

1. Department of Applied Aerodynamics, ONERA—The French Aerospace Lab, 92190 Meudon, France

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference46 articles.

1. Challenges of future aircraft propulsion: A review of distributed propulsion technology and its potential application for the all electric commercial aircraft

2. AshcraftS. W.PadronA. S.PascioniK. A.StoutG. W.Jr.HuffD. L. “Review of Propulsion Technologies for N+3 Subsonic Vehicle Concepts,” NASA TM-2011-217239, 2011.

3. Progress in Astronautics and Aeronautics;Covert E. E.,1985

4. StolikerF. N. “Guide to In-Flight Thrust Measurement of Turbojets and Fan Engines,” Advisory Group for Aerospace Research and Development, Ministry-Industry Drag Analysis Panel Study Group, AG-237, 1979.

5. KawaiR. T.FriedmanD.SerranoL. “Blended Wing Body (BWB) Boundary Layer Ingestion (BLI) Inlet Configuration and System Studies,” NASA CR-2006-214534, 2006.

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