Diode-Laser Sensor for Air-Mass Flux 2: Non-Uniform Flow Modeling and Aeroengine Tests
Author:
Affiliation:
1. Stanford University, Stanford, California 94305
2. Pratt and Whitney Aircraft, United Technologies Corporation, East Hartford, Connecticut 06108
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.27683
Reference9 articles.
1. Diode-Laser Sensor for Air-Mass Flux 1: Design and Wind Tunnel Validation
2. Steady Performance Measurements of a Turbofan Engine With Inlet Distortions Containing Co- and Counterrotating Swirl From an Intake Diffuser for Hypersonic Flight
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