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Volumn , Issue , 2010, Pages

Integrated Aero-Servo-Thermo-Propulso-Elasticity (ASTPE) methodology for hypersonic scramjet vehicle design/analysis

Author keywords

[No Author keywords available]

Indexed keywords

DESIGN ENVIRONMENT; DESIGN PROCEDURE; DESIGN/ANALYSIS; MULTI-DISCIPLINARY; PRELIMINARY DESIGN; RAPID ASSESSMENT; SEM; VEHICLE DESIGN;

EID: 78649834402     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (8)

References (28)
  • 1
    • 0032656280 scopus 로고    scopus 로고
    • Simple analytical model for parametric studies of hypersonic waveriders
    • July-August
    • Starkey, R.P., and Lewis, M. J., "Simple Analytical Model for Parametric Studies of Hypersonic Waveriders," AIAA Journal of Spacecraft and Rockets, Volume 36, Number 4, July-August 1999, pages 516-523.
    • (1999) AIAA Journal of Spacecraft and Rockets , vol.36 , Issue.4 , pp. 516-523
    • Starkey, R.P.1    Lewis, M.J.2
  • 2
    • 0026406416 scopus 로고
    • Design and modeling issues for integrated airframe/propulsion control of hypersonic flight vehicles
    • Paper WP7, Boston, MA
    • McRuer, D., "Design and Modeling Issues for Integrated Airframe/Propulsion Control of Hypersonic Flight Vehicles," Paper WP7, 1991 American Control Conference, Boston, MA, 1991. pp. 729-735.
    • (1991) 1991 American Control Conference , pp. 729-735
    • McRuer, D.1
  • 3
    • 78649874092 scopus 로고    scopus 로고
    • AIAA HyTASP Program Committee, Technical Fellowship Advisory Board Study, December 18
    • Bowcutt, K. G., "Hypersonic technology Status and Development Roadmap," AIAA HyTASP Program Committee, Technical Fellowship Advisory Board Study, December 18, 2003.
    • (2003) Hypersonic Technology Status and Development Roadmap
    • Bowcutt, K.G.1
  • 4
    • 0028546482 scopus 로고
    • Analytical aeropropulsive/aeroelastic hypersonic-vehicle model with dynamic analysis
    • November-December
    • Chavez, F. R., and Schmidt, D. K., "Analytical Aeropropulsive/ Aeroelastic Hypersonic-Vehicle Model with Dynamic Analysis," Journal of Guidance, Control & Dynamics, Vol. 17, No. 6, November-December 1994, pp. 1308-1319.
    • (1994) Journal of Guidance, Control & Dynamics , vol.17 , Issue.6 , pp. 1308-1319
    • Chavez, F.R.1    Schmidt, D.K.2
  • 5
    • 0037278917 scopus 로고    scopus 로고
    • Sensitivity of hydrocarbon combustion modeling for hypersonic missile design
    • Jan-Feb
    • Starkey, R. P., and Lewis, M. J., "Sensitivity of Hydrocarbon Combustion Modeling for Hypersonic Missile Design," AIAA Journal of Propulsion and Power, Vol. 19, No. 1, Jan-Feb 2003, pp. 89-97.
    • (2003) AIAA Journal of Propulsion and Power , vol.19 , Issue.1 , pp. 89-97
    • Starkey, R.P.1    Lewis, M.J.2
  • 6
    • 78649868175 scopus 로고    scopus 로고
    • ZONA Technology, Inc. and University of Maryland, AF STTR Phase I Proposal, Topic # AF05-T027, Proposal # F054-027-0129, Submitted August 10
    • ZONA Technology, Inc. and University of Maryland, "Integrated Aero-Servo-Thermo-Populso-Elasticity (ASTPE) for Hypersonic Scramjet Vehicle Design/Analysis," AF STTR Phase I Proposal, Topic # AF05-T027, Proposal # F054-027-0129, Submitted August 10, 2005.
    • (2005) Integrated Aero-Servo-Thermo-Populso-Elasticity (ASTPE) for Hypersonic Scramjet Vehicle Design/Analysis
  • 8
    • 29744439758 scopus 로고    scopus 로고
    • A non-linear model for the longitudinal dynamics of a hypersonic air-breathing vehicle
    • AIAA 200-6255, 15-18 August, San Francisco, CA
    • Boldender, M.A., and Doman, D.B., "A Non-Linear Model for the Longitudinal Dynamics of a Hypersonic Air-Breathing Vehicle," AIAA 200-6255, AIAA Guideance, Navigation, and Control Conference and Exhibit, 15-18 August 2005, San Francisco, CA.
    • (2005) AIAA Guideance, Navigation, and Control Conference and Exhibit
    • Boldender, M.A.1    Doman, D.B.2
  • 14
    • 0035509541 scopus 로고    scopus 로고
    • Quasi-one-dimensional high speed engine model with finite rate chemistry
    • Nov-Dec
    • O'Brien, T. F., Starkey, R. P., and Lewis, M. J., "Quasi-One- Dimensional High Speed Engine Model With Finite Rate Chemistry," AIAA Journal of Propulsion and Power, Vol. 17, No. 6, Nov-Dec 2001, pp. 1366-1374.
    • (2001) AIAA Journal of Propulsion and Power , vol.17 , Issue.6 , pp. 1366-1374
    • O'Brien, T.F.1    Starkey, R.P.2    Lewis, M.J.3
  • 18
    • 0033885972 scopus 로고    scopus 로고
    • Joint Jet-A/silane/hydrgoen reation mechanism
    • Lewis, M.J., and Chang, J.S., "Joint Jet-A/Silane/Hydrgoen Reation Mechanism," Journal of Propulsion and Power, Vol. 16, No. 2, 2000. pp.365-367.
    • (2000) Journal of Propulsion and Power , vol.16 , Issue.2 , pp. 365-367
    • Lewis, M.J.1    Chang, J.S.2
  • 21
    • 77958466680 scopus 로고    scopus 로고
    • Off-design performance characterization of a variable geometry scramjet
    • ISABE-2005-1111, September 4-9, Munich, Germany
    • Starkey, R. P., "Off-design Performance Characterization of a Variable Geometry Scramjet," ISABE-2005-1111, 17th International Symposium on Airbreathing Engines, September 4-9, 2005, Munich, Germany.
    • (2005) 17th International Symposium on Airbreathing Engines
    • Starkey, R.P.1
  • 22
    • 0004230787 scopus 로고
    • Addison-Wesley Publishing Company, Inc. Reading, Massachusetts, Ch. 4
    • Bisplinghoff, R. L., Ashley, H., and Halfman, R. L., " Aeroelasticity," Addison-Wesley Publishing Company, Inc. Reading, Massachusetts, 1957, Ch. 4.
    • (1957) Aeroelasticity
    • Bisplinghoff, R.L.1    Ashley, H.2    Halfman, R.L.3
  • 24
    • 0003771178 scopus 로고    scopus 로고
    • Application of multivariable control theory to aircraft control laws
    • Wright-Patterson AFB, OH 45433-7562, May
    • Wright laboratory Report WL-TR-96-3099, "Application of Multivariable Control Theory to Aircraft Control Laws," Wright-Patterson AFB, OH 45433-7562, May 1996.
    • (1996) Wright Laboratory Report WL-TR-96-3099
  • 25
    • 0003096706 scopus 로고
    • Dynamic inversion: An evolving methodology for flight control design
    • Enns, D., Bugajski, D., Hendrick, R., and Stein, G., "Dynamic Inversion: An Evolving Methodology for Flight Control Design," Int. Journal of Control, 1994, Vol. 59, No.1, pp. 71-91.
    • (1994) Int. Journal of Control , vol.59 , Issue.1 , pp. 71-91
    • Enns, D.1    Bugajski, D.2    Hendrick, R.3    Stein, G.4
  • 26
    • 20344396363 scopus 로고    scopus 로고
    • On improving efficiency of differential evolution for aerodynamic shape optimization applications
    • AIAA Paper No. 2004-778, Albany, NY, Aug
    • Madavan, N. K., "On Improving Efficiency of Differential Evolution for Aerodynamic Shape Optimization Applications," AIAA Paper No. 2004-778, 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, Albany, NY, Aug 2004.
    • (2004) 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference
    • Madavan, N.K.1
  • 27
    • 0004081663 scopus 로고    scopus 로고
    • Vanderplaats Research & Development, Inc. version 5.0. Colorado Springs, CO
    • Vanderplaats Research & Development, Inc. DOT Users Manual, version 5.0. Colorado Springs, CO, 1999.
    • (1999) DOT Users Manual
  • 28
    • 85043996274 scopus 로고    scopus 로고
    • Aerodynamic shape optimization using hybridized differential evolution
    • AIAA Paper No. 2003-3792, Orlando, FL, June
    • Madavan, N. K., "Aerodynamic Shape Optimization Using Hybridized Differential Evolution," AIAA Paper No. 2003-3792, 21st Applied Aerodynamics Conference, Orlando, FL, June 2003.
    • (2003) 21st Applied Aerodynamics Conference
    • Madavan, N.K.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.