Verification and analysis of Formulation 4 of Langley for the study of noise from high speed surfaces
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. Midwestern State Univ., Wichita Falls, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1881
Reference22 articles.
1. Sound generation by turbulence and surfaces in arbitrary motion
2. Farassat,F. "Theory of noise generationfrom moving bodies with an application to helicopter rotors0022, NASA TR R-45X (1975), (Available at http://techreports.larc.nasa.gov/ltrs/PDFmASA-75trr451.pdfi
3. Brentner, Kenneth S. "Prediction of helicopter rotor discrete frequency noise-A computer program incorporating realistic blade motions and advanced acoustic formulation0022, NASA Technical Memorandum 87721(1986)
4. Advanced turboprop noise prediction based on recent theoretical results
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