The Effect of Bypass Nozzle Exit Area on Fan Aerodynamic Performance and Noise in a Model Turbofan Simulator

By National Aeronautics and Space Administration

Technical Report Hughes, Christopher E. and Podboy, Gary, G. and Woodward, Richard P. and Jeracki, Robert, J. Glenn Research Center NASA/TM-2013-214029, GT2005-68573, E-15384 WBS 22-781-30-75 NOISE REDUCTION; TURBOFAN ENGINES; AEROACOUSTICS; AERODYNAMIC NOISE; FAN BLADES; AERODYNAMIC CHARACTERISTICS; FAR FIELDS; NOZZLE FLOW; AIRCRAFT NOISE; LOW SPEED WIND TUNNELS; LASER DOPPLER VELOCIMETERS; SCALE MODELS

• Format: Paperback
• Language: English
• ISBN: B08F65SB46
• ISBN13: 9798673171509
• Release Date: January 1
• Publisher: Independently Published
• Length: 42 Pages
• Weight: 0.27 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"