Applications of Response Surface-Based Methods to Noise Analysis in the Conceptual Design of Revolutionary Aircraft

Collection of Technical Papers - 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference

Volumn 3, Issue , 2004, Pages 1556-1567

  Hill, Geoffrey A ^a,b   Olson, Erik D ^a,b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Systems Analysis Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACOUSTIC NOISE; ACOUSTIC WAVES; AIR TRANSPORTATION; OPTIMIZATION; PARAMETER ESTIMATION; POLYNOMIAL APPROXIMATION; PRODUCT DESIGN; WINGS;

BLENDED-WING-BODY (BWB); CONCEPTUAL DESIGN; RESPONSE SURFACE-BASED METHODS; TRADE SPACE;

AIRCRAFT;

EID: 20344402318     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-4437     Document Type: Conference Paper

References (13)

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2. Dagget, David L., Kawai, Ron, and Friedman, Doug, "Blended Wing Body Systems Studies: Boundary Layer Ingestion Inlets With Active Flow Control," NASA/CR-2003-212670, 2003.
3. DOT/FAA Noise Standards: Aircraft Type and Airworthiness Certification, FAR Part 36, June 9, 2004.
4. Zorumski, William E., "Aircraft Noise Prediction Program Theoretical Manual," NASA TM-83199, 1982.
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9. th International Council of the Aeronautical Sciences (ICAS) Congress, Sorrento, Italy, September 8-13, 1996.
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11. Olson, Erik D., and Mavris, Dimitri N., "Development of Response Surface Equations for High-Speed Civil Transport Takeoff and Landing Noise," AIAA Paper No. 97-5570, 1997.
12. Antoine, Nicolas E., and Kroo, Ilan M., "Optimizing Aircraft and Operations for Minimum Noise," AIAA Paper No. 2002-5868, 2002.
13. Mavris, Dimitri N., and Kirby, Michelle R., "Technology Identification, Evaluation, and Selection for Commercial Transport Aircraft," SAWE Paper No. 2456, 1999.