The beneficial effects of wing dihedral on sonic boom

9th AIAA/CEAS Aeroacoustics Conference and Exhibit

Volumn , Issue , 2003, Pages

  Bobbitt, P J ^a   Kandil, O A ^b   Yang, Z ^b  

^a Eagle Aeronautics Inc   (United States)

^b Old Dominion University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894562634     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (24)

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2. Jones, L. B.: Lower Bounds for Sonic Bang in the Far Field. Aeron. Quart. XVIII, Pt. 1, 1-21 (1967).
3. Seebass, R.: Minimum Sonic Boom Shock Strengths and Overpressures. Nature 221, 651-653 (1969)
4. Jones, L. B.: Lower Bounds for the Pressure Jump of the Bow Shock of a Supersonic Transport. The Acoustical Quarterly, Vol. XXI, Feb. 1970.
5. George, A. R.; and Seebass, R.: Sonic Boom Minimization Including Both Front and Real Shocks. AIAA J. 9, 2091-2093 (1971).
6. Seebass, R.; and George, A. R.: Sonic-Boom Minimization. J. Acoust. Soc. Am., Vol. 51, No. 2 (pt. 3), Feb. 1972, pp. 686-694.
7. Ferri, Antonio; and Schwartz, Ira R.: Sonic Boom Generation, Propagation, and Minimization. AIAA Paper No. 72-194, Jan. 1972.
8. Carlson, Harry W., Barger, Raymond L.; and Mack, Robert J.: Application of Sonic-Boom Minimization Concepts in Supersonic Transport Design. NASA TN-D-7218, 1973.
9. Darden, Christine, M.: Minimization of Sonic-Boom Parameters in Real and Isothermal Atmospheres. NASA TN D- 7842, 1975.
10. Darden, Christine M.: Sonic Boom Minimization With Nose-Bluntness Relaxation. NASA TP 1348, Jan. 1979.
11. Mack, Robert J.; and Darden, Christine M.: Wind-Tunnel Investigation of the Validity of a Sonic-Boom-Minimization Concept. NASA TP 1421. October 1979.
12. Hague, D. S.; and Jones, R. T.: Application of Multivariable Search Techniques to a Design of Low Sonic Boom Overpressure Body Shapes. NASA SP-255, pp. 307-323, Oct. 1970.
13. Haglund, George T.: High Speed Civil Transport Design for Reduced Sonic Boom. Boeing Doc. No. D6-55430, NASA Cont. No. NAS1-18377, (1991)
14. Mack, Robert J.; and Haglund, George T.: A Practical Low-Boom Overpressure Signature Based on Minimum Sonic Boom Theory. NASA C P- 3173, Vol. II, pp. 15-19, Feb. 1992.
15. Mack, Robert J.: Additional F-Functions Useful for Preliminary Design of Shaped Signature, Low-Boom, Supersonic-Cruise Aircraft. NASA CDCP-1001, pp. 1-12, Oct. 1994.
16. Hunton, Lynn W.: Current Research in Sonic Boom. NASA SP-180, pp. 57-66, May 1968.
17. Bobbitt, Percy J.: Application of Computational Fluid Dynamics and Laminar Flow Technology for Improved Performance and Sonic Boom Reduction. NASA CP 3173, Vol. II, Feb. 1992.
18. Kandil, O. A.; Yang, Z.; Bobbitt, P. J.: Prediction of Sonic Boom Signature Using Euler-Full Potential CFD with Grid Adaptation and Shock Fitting. AIAA CP 2002-2543, June 2002.
19. Goodsell, Aga M.; Lee, Christopher A.; and Hicks, Raymond M.: Use of CFD in the Design of Low Sonic Boom Aircraft. NASA CP 10133, Vol. II, pp. 143-168. May 1993.
20. Haglund, George T.: Potential for Sonic Boom Reduction of the Boeing HSCT. CFCP-1003, Vol. II, pp. 96-120. July 1996.
21. Morgenstrn, John M.: Potential for Sonic Boom Reduction of the 2.4 H5085 Arrow Wing HSCT. NASA CDCP-1003, Vol. II, pp. 162-175, July 1996.
22. Thomas, Charles L.: Extrapolation of Sonic Boom Pressure Signatures by the Waveform Parameter Method. NASA TN-D-6832, June 1972.
23. Thomas, Charles L.: Extrapolation of Wind- Tunnel Sonic Boom Signatures Without Use of a Whitham F-Function. Third Conf. on Sonic Boom Research. NASA SP-255, Oct. 29-30, 1970.
24. Meteorological Aspects of the Sonic Boom. Prepared by The Boeing Company, under Contract FA-WA-4717. SRDS Rept. No. RD-64-160. Sept. 1964.