1. 1Hayes,J.A.,Horne,W.C.,Soderman,P.T.,andBent,P.H.“AirframeNoiseCharacteristicsofa4.7%ScaleDC-10Model,”1997.
2. 2Storms,B.L.,Ross,J.C.,Horne,W.,Hayes,J.,Dougherty,R.P.,Underbrink,J.R.,Scharpf,D.F.,andMoriarty,P.J.“AnAeroacousticStudy ofanUnsweptWingwithaThree-DimensionalHighLiftSystem,”NASATM112222,February1998.
3. 3Dobrzynski,W.,Nagakura,K.,Gehlhar,B.,andBuschbaum,A.“AirframeNoiseStudiesonWingswithDeployedHigh-LiftDevices,”AIAA Paper1998-2337,1998.
4. 4Storms, B. L., Hayes, J. A., Moriarty, P. J., and Ross, J. C. “Aeroacoustic Measurements of Slat Noise on a Three-Dimensional High-Lift System,”AIAAPaper1999-1957,1999.
5. 5Choudhari, M.M., Lockard, D.P., Macaraeg, M.G., Singer, B.A., Streett, C. L., Neubert, G. R., Stoker, R. W., Underbrink, J. R., Berkman, M. E., Khorrami, M. R., and Sadowski, S. S. “Aeroacoustic Experiments in the Langley Low-Turbulence Pressure Tunnel,” NASA TM-211432, February2002.