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Volumn , Issue , 2005, Pages 3773-3782

Improved sonic boom minimization with extendable nose spike

Author keywords

[No Author keywords available]

Indexed keywords

BUSINESS JETS; SONIC BOOMS; SUPERSONIC FLIGHTS;

EID: 30744444965     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (57)

References (18)
  • 6
    • 78149440264 scopus 로고
    • Some nonasymptotic effects of the sonic boom of large airplanes
    • June
    • McLean, F.E., "Some Nonasymptotic Effects of the Sonic Boom of Large Airplanes," NASA TN D-2877, June 1965.
    • (1965) NASA TN , vol.D-2877
    • McLean, F.E.1
  • 7
    • 85006409852 scopus 로고
    • Sonic boom minimization including both front and rear shocks
    • George, A. R., and Seebass, R., "Sonic Boom Minimization Including Both Front and Rear Shocks," AIAA Journal, Vol. 9, No. 10, 1971, pp. 2091-2903.
    • (1971) AIAA Journal , vol.9 , Issue.10 , pp. 2091-2903
    • George, A.R.1    Seebass, R.2
  • 9
    • 5244239198 scopus 로고
    • Minimization of sonic boom parameters in real and isothermal atmospheres
    • Darden, C. M., "Minimization of Sonic Boom Parameters in Real and Isothermal Atmospheres," NASA TN D-7842, 1975.
    • (1975) NASA TN , vol.D-7842
    • Darden, C.M.1
  • 10
    • 20344380890 scopus 로고
    • Sonic-boom minimization with nose bluntness relaxation
    • Darden, C. M., "Sonic-Boom Minimization with Nose Bluntness Relaxation," NASA TP 1348, 1979.
    • (1979) NASA TP , vol.1348
    • Darden, C.M.1
  • 11
    • 30744460852 scopus 로고
    • Low-boom aircraft concept with aft-fuselage mounted engine nacelles
    • NASA CP-10133, May
    • Mack, R. J., Low-Boom Aircraft Concept with Aft-Fuselage Mounted Engine Nacelles," 1993 - High Speed Research: Sonic Boom, Volume II, NASA CP-10133, May 1993.
    • (1993) 1993 - High Speed Research: Sonic Boom, Volume II , vol.2
    • Mack, R.J.1
  • 12
    • 0018529839 scopus 로고
    • Wind tunnel investigation of the validity of a sonic boom minimization concept
    • Mack, R. J., and Darden C. M., "Wind Tunnel Investigation of the Validity of a Sonic Boom Minimization Concept," NASA TP-1421, 1979.
    • (1979) NASA TP-1421
    • Mack, R.J.1    Darden, C.M.2
  • 13
    • 2942748978 scopus 로고
    • Extrapolation of sonic boom pressure signatures by the waveform parameter method
    • June
    • Thomas, C. L., "Extrapolation of Sonic Boom Pressure Signatures by the Waveform Parameter Method," NASA TN D-6832, June 1972.
    • (1972) NASA TN , vol.D-6832
    • Thomas, C.L.1
  • 14
    • 84888808932 scopus 로고    scopus 로고
    • Gulfstream Aerospace Corporation, Savannah, GA, U.S. Patent for a "Supersonic Aircraft with Spike for Controlling and Reducing Sonic Boom, Patent No. US 6,698,684 B1, March 2
    • Henne, P. A., Howe, D. C., Wolz, R. R., and Hancock, J. L., Gulfstream Aerospace Corporation, Savannah, GA, U.S. Patent for a "Supersonic Aircraft with Spike for Controlling and Reducing Sonic Boom," Patent No. US 6,698,684 B1, March 2, 2004.
    • (2004)
    • Henne, P.A.1    Howe, D.C.2    Wolz, R.R.3    Hancock, J.L.4
  • 15
    • 85040284939 scopus 로고
    • Description and calibration of the langley unitary plan wind tunnel
    • November
    • Jackson, C. M., Corlett, W. A. and Monta, W. J., "Description and Calibration of the Langley Unitary Plan Wind Tunnel," NASA TP-1905, November 1981.
    • (1981) NASA TP-1905
    • Jackson, C.M.1    Corlett, W.A.2    Monta, W.J.3
  • 16
    • 30744468297 scopus 로고    scopus 로고
    • NASA Langley Research Center, Hampton, VA
    • Overflow Software Package, Ver. 2.0y, NASA Langley Research Center, Hampton, VA, 2004.
    • (2004) Overflow Software Package, Ver. 2.0y


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.