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Volumn 29, Issue 3, 2013, Pages 610-620

Mission-integrated exergy analysis for hypersonic vehicles: Methodology and application

Author keywords

[No Author keywords available]

Indexed keywords

ENTROPY; EXERGY; HYPERSONIC AERODYNAMICS; PROPULSION; WAKES;

EID: 84878339253     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/1.B34733     Document Type: Article
Times cited : (20)

References (28)
  • 1
    • 84873816637 scopus 로고    scopus 로고
    • Characterization of aerospace vehicle performance and mission analysis using exergy
    • Progress in Astronautics and Aeronautics, AIAA, Reston, VA
    • Riggins, D.W., Camberos, J., and Moorhouse, D., "Characterization of Aerospace Vehicle Performance and Mission Analysis Using Exergy," Exergy Analysis and Design Optimization for Aerospace Vehicles and Systems, Vol. 238, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2011, pp. 275-307.
    • (2011) Exergy Analysis and Design Optimization for Aerospace Vehicles and Systems , vol.238 , pp. 275-307
    • Riggins, D.W.1    Camberos, J.2    Moorhouse, D.3
  • 3
    • 77953144217 scopus 로고
    • General equations and theorems
    • Academic Press, New York
    • Oswatitsch, K., "General Equations and Theorems," Gas Dynamics, Academic Press, New York, 1956, pp. 177-210.
    • (1956) Gas Dynamics , pp. 177-210
    • Oswatitsch, K.1
  • 4
    • 0032687203 scopus 로고    scopus 로고
    • Wake integration for three- dimensional flowfield computations: Theoretical development
    • doi:10.2514/2.2465
    • Giles, M., and Cummings, R., "Wake Integration for Three- Dimensional Flowfield Computations: Theoretical Development," Journal of Aircraft, Vol. 36, No. 2, 1999, pp. 357-365. doi:10.2514/2.2465
    • (1999) Journal of Aircraft , vol.36 , Issue.2 , pp. 357-365
    • Giles, M.1    Cummings, R.2
  • 5
    • 0032633634 scopus 로고    scopus 로고
    • Wake integration for three-dimensional flowfield computations: Applications
    • doi:10.2514/2.2466
    • Hunt, D., Giles, M., and Cummings, R., "Wake Integration for Three-Dimensional Flowfield Computations: Applications," Journal of Aircraft, Vol. 36, No. 2, 1999, pp. 366-373. doi:10.2514/2.2466
    • (1999) Journal of Aircraft , vol.36 , Issue.2 , pp. 366-373
    • Hunt, D.1    Giles, M.2    Cummings, R.3
  • 6
    • 33748077798 scopus 로고    scopus 로고
    • Methodology for performance analysis of aerospace vehicles using the laws of thermodynamics
    • doi:10.2514/1.16426
    • Riggins, D. W., Taylor, T., and Moorhouse, D., "Methodology for Performance Analysis of Aerospace Vehicles Using the Laws of Thermodynamics," Journal of Aircraft, Vol. 43, No. 4, 2006, pp. 953- 963. doi:10.2514/1.16426
    • (2006) Journal of Aircraft , vol.43 , Issue.4 , pp. 953-963
    • Riggins, D.W.1    Taylor, T.2    Moorhouse, D.3
  • 8
    • 84873801250 scopus 로고    scopus 로고
    • Optimization utilizing entropy-generation minimization for maximum performance of hypersonic vehicles
    • Progress in Astronautics and Aeronautics, AIAA, Reston, VA
    • Riggins, D.W., Moorhouse, D., Camberos, J., and von Spakovsky, M., "Optimization Utilizing Entropy-Generation Minimization for Maximum Performance of Hypersonic Vehicles," Exergy Analysis and Design Optimization for Aerospace Vehicles and Systems, Vol. 238, Progress in Astronautics and Aeronautics, AIAA, Reston, VA, 2011, pp. 229-273.
    • (2011) Exergy Analysis and Design Optimization for Aerospace Vehicles and Systems , vol.238 , pp. 229-273
    • Riggins, D.W.1    Moorhouse, D.2    Camberos, J.3    Von Spakovsky, M.4
  • 9
    • 77953157750 scopus 로고    scopus 로고
    • The characterization of aerospace vehicle performance and mission analysis using thermodynamic availability
    • doi:10.2514/1.46420
    • Riggins, D. W., Camberos, J., and Moorhouse, D., "The Characterization of Aerospace Vehicle Performance and Mission Analysis Using Thermodynamic Availability," Journal of Aircraft, Vol. 47, No. 3, 2010, pp. 904-916. doi:10.2514/1.46420
    • (2010) Journal of Aircraft , vol.47 , Issue.3 , pp. 904-916
    • Riggins, D.W.1    Camberos, J.2    Moorhouse, D.3
  • 11
    • 33744991884 scopus 로고
    • Elements of Flight Propulsion, Wiley, New York
    • Foa, J., "Efficiencies-Propulsive Cycles," Elements of Flight Propulsion, Wiley, New York, 1960, pp. 274-287.
    • (1960) Efficiencies-Propulsive Cycles , pp. 274-287
    • Foa, J.1
  • 13
    • 1542501574 scopus 로고    scopus 로고
    • The thermodynamic continuum of jet engine performance: The principle of lost work due to irreversibility in aerospace systems
    • Riggins, D. W., "The Thermodynamic Continuum of Jet Engine Performance: The Principle of Lost Work Due to Irreversibility in Aerospace Systems," International Journal of Thermodynamics, Vol. 6, No. 3, 2003, pp. 107-120.
    • (2003) International Journal of Thermodynamics , vol.6 , Issue.3 , pp. 107-120
    • Riggins, D.W.1
  • 14
    • 0016940712 scopus 로고
    • Propulsive efficiency from an energy utilization standpoint
    • doi:10.2514/3.44525
    • Lewis, J. H., "Propulsive Efficiency from an Energy Utilization Standpoint," Journal of Aircraft, Vol. 13, No. 4, 1976, pp. 299-302. doi:10.2514/3.44525
    • (1976) Journal of Aircraft , vol.13 , Issue.4 , pp. 299-302
    • Lewis, J.H.1
  • 16
    • 0031099209 scopus 로고    scopus 로고
    • Thrust losses in hypersonic engines part 1: Methodology
    • doi:10.2514/2.5160
    • Riggins, D., McClinton, C. R., and Vitt, P., "Thrust Losses in Hypersonic Engines Part 1: Methodology," Journal of Propulsion and Power, Vol. 13, No. 2, 1997, pp. 281-287. doi:10.2514/2.5160
    • (1997) Journal of Propulsion and Power , vol.13 , Issue.2 , pp. 281-287
    • Riggins, D.1    McClinton, C.R.2    Vitt, P.3
  • 17
    • 0031098509 scopus 로고    scopus 로고
    • Thrust losses in hypersonic engines part 2: Applications
    • doi:10.2514/2.5161
    • Riggins, D., "Thrust Losses in Hypersonic Engines Part 2: Applications," Journal of Propulsion and Power, Vol. 13, No. 2, 1997, pp. 288-295. doi:10.2514/2.5161
    • (1997) Journal of Propulsion and Power , vol.13 , Issue.2 , pp. 288-295
    • Riggins, D.1
  • 18
    • 0035279033 scopus 로고    scopus 로고
    • Comparison of thermodynamic loss models suitable for gas turbine propulsion
    • doi:10.2514/2.5745
    • Roth, B., "Comparison of Thermodynamic Loss Models Suitable for Gas Turbine Propulsion," Journal of Propulsion and Power, Vol. 17, No. 2, 2001, pp. 324-332. doi:10.2514/2.5745
    • (2001) Journal of Propulsion and Power , vol.17 , Issue.2 , pp. 324-332
    • Roth, B.1
  • 19
    • 0036867812 scopus 로고    scopus 로고
    • A work potential perspective of engine component performance
    • doi:10.2514/2.6077
    • Roth, B., "A Work Potential Perspective of Engine Component Performance," Journal of Propulsion and Power, Vol. 18, No. 6, 2002, pp. 1183-1190. doi:10.2514/2.6077
    • (2002) Journal of Propulsion and Power , vol.18 , Issue.6 , pp. 1183-1190
    • Roth, B.1
  • 20
    • 0016540115 scopus 로고
    • Availability and propulsion
    • doi:10.1243/JMES-JOUR-1975-017-033-02
    • Clarke, J., and Horlock, J., "Availability and Propulsion," Journal of Mechanical Engineering Science, Vol. 17, No. 4, 1975, pp. 223-232. doi:10.1243/JMES-JOUR-1975-017-033-02
    • (1975) Journal of Mechanical Engineering Science , vol.17 , Issue.4 , pp. 223-232
    • Clarke, J.1    Horlock, J.2
  • 21
    • 0343705817 scopus 로고
    • Energy analysis of high-speed flight systems
    • edited by Curran, T., and Murthy, S., Progress in Astronautics and Aeronautics, AIAA, Washington, DC
    • Czysz, P., and Murthy, S., "Energy Analysis of High-Speed Flight Systems," High-Speed Flight Propulsion Systems, edited by Curran, T., and Murthy, S., Vol. 137, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1991, pp. 143-236.
    • (1991) High-Speed Flight Propulsion Systems , vol.137 , pp. 143-236
    • Czysz, P.1    Murthy, S.2
  • 22
    • 0031097942 scopus 로고    scopus 로고
    • Evaluation of performance loss methods for high-speed engines and engine components
    • doi:10.2514/2.5162
    • Riggins, D., "Evaluation of Performance Loss Methods for High-Speed Engines and Engine Components," Journal of Propulsion and Power, Vol. 13, No. 2, 1997, pp. 296-304. doi:10.2514/2.5162
    • (1997) Journal of Propulsion and Power , vol.13 , Issue.2 , pp. 296-304
    • Riggins, D.1
  • 25
    • 4944260299 scopus 로고    scopus 로고
    • Analysis of the magneto-hydrodynamic (mhd) energy bypass engine for high-speed air-breathing propulsion
    • doi:10.2514/1.4980
    • Riggins, D. W., "Analysis of the Magneto-Hydrodynamic (MHD) Energy Bypass Engine for High-Speed Air-Breathing Propulsion," Journal of Propulsion and Power, Vol. 20, No. 5, 2004, pp. 779-792. doi:10.2514/1.4980
    • (2004) Journal of Propulsion and Power , vol.20 , Issue.5 , pp. 779-792
    • Riggins, D.W.1
  • 26
    • 79961098845 scopus 로고    scopus 로고
    • X-43-scramjet power breaks the hypersonic barrier
    • AIAA Paper 2006- 1, Jan.
    • McClinton, C. R., "X-43-Scramjet Power Breaks the Hypersonic Barrier," Dryden Lectureship in Research for 2006, AIAA Paper 2006- 1, Jan. 2006.
    • (2006) Dryden Lectureship in Research for 2006
    • McClinton, C.R.1
  • 27
    • 1842472615 scopus 로고
    • Prentice-Hall, Upper Saddle River, NJ
    • Hall, N., and Ibele, W., Engineering Thermodynamics, Prentice-Hall, Upper Saddle River, NJ, 1960, pp. 378-446.
    • (1960) Engineering Thermodynamics , pp. 378-446
    • Hall, N.1    Ibele, W.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.