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Volumn , Issue , 2001, Pages

Two-step linear regression method for identification of high incidence unsteady aerodynamic model

Author keywords

[No Author keywords available]

Indexed keywords


EID: 79551678908     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (24)

References (11)
  • 2
    • 0028498390 scopus 로고
    • State- Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack
    • Sept.-Oct
    • Goman, M.G., and A.N. Khrabrov. "State- Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack," Journal of Aircraft, Vol.31, No.5, Sept.-Oct. 1994, pp.1109-1115.
    • (1994) Journal of Aircraft , vol.31 , Issue.5 , pp. 1109-1115
    • Goman, M.G.1    Khrabrov, A.N.2
  • 3
    • 4244020891 scopus 로고    scopus 로고
    • Difficulties in the Application of Stability Derivatives to the Manoeuvring Aerodynamics of Combat Aircraft
    • 1C AS Paper 98-1.7.1, Sept, Melbourne, Australia
    • Greenwell, D.I. "Difficulties in the Application of Stability Derivatives to the Manoeuvring Aerodynamics of Combat Aircraft," 1C AS Paper 98-1.7.1, The 21th Congress of the Aeronautical Sciences, Sept. 1998, Melbourne, Australia.
    • (1998) The 21th Congress of the Aeronautical Sciences
    • Greenwell, D.I.1
  • 4
    • 19644387050 scopus 로고    scopus 로고
    • The Characteristic Time Constant Approach for Mathematical Modelling of High Angle of Attack Aerodynamics
    • ICAS Paper, Sept, Harrogate, UK, 223.1-223.14
    • Goman, M.G., Greenwell, D.L, and A.N. Khrabrov. "The Characteristic Time Constant Approach for Mathematical Modelling of High Angle of Attack Aerodynamics", ICAS Paper, 22nd Congress of the Aeronautical Sciences, Sept. 2000, Harrogate, UK, pp. 223.1-223.14.
    • (2000) 22nd Congress of the Aeronautical Sciences
    • Goman, M.G.1    Greenwell, D.L.2    Khrabrov, A.N.3
  • 5
    • 84894366128 scopus 로고    scopus 로고
    • Simple Wings Unsteady Aerodynamics at High Angles of Attack: Experimental and Modeling Results
    • August, Portland, OR
    • Abramov, N.B., Goman, M.G., Khrabrov, A.N., and K.A. Kolinko "Simple Wings Unsteady Aerodynamics at High Angles of Attack: Experimental and Modeling Results," Paper 99-4013, AIAA Atmospheric Flight Mechanics Conference, August 1999, Portland, OR.
    • (1999) AIAA Atmospheric Flight Mechanics Conference , pp. 99-4013
    • Abramov, N.B.1    Goman, M.G.2    Khrabrov, A.N.3    Kolinko, K.A.4
  • 6
    • 0041993346 scopus 로고    scopus 로고
    • Part 1 - Postulated Models, NASA TM 109120, May 1994; Part 2 - Parameters Estimated From Wind Tunnel Data, NASA TM 110161, April 1995; Part 3 - Parameters Estimated From Flight Data, NASA TM 110259, May
    • Klein, V., and Noderer, K.D. "Modeling of Aircraft Unsteady Aerodynamic Characteristics," Part 1 - Postulated Models, NASA TM 109120, May 1994; Part 2 - Parameters Estimated From Wind Tunnel Data, NASA TM 110161, April 1995; Part 3 - Parameters Estimated From Flight Data, NASA TM 110259, May 1996.
    • (1996) Modeling of Aircraft Unsteady Aerodynamic Characteristics
    • Klein, V.1    Noderer, K.D.2
  • 8
    • 0006718304 scopus 로고    scopus 로고
    • Airload Prediction for Delta Wings at High Incidence
    • ICAS Paper, Sept, Harrogate, UK, 221.1-221.10
    • Huang, X.Z., Lou, H.Y., and E.S. Hanf "Airload Prediction for Delta Wings at High Incidence", ICAS Paper, 22nd Congress of the Aeronautical Sciences, Sept. 2000, Harrogate, UK, pp. 221.1-221.10.
    • (2000) 22nd Congress of the Aeronautical Sciences
    • Huang, X.Z.1    Lou, H.Y.2    Hanf, E.S.3
  • 9
    • 84983168518 scopus 로고    scopus 로고
    • Time History Effects On a Rolling 65 Deg Delta-Wing-Body Configuration
    • Paper 97-3645, August, New Orleans, LA
    • Ericsson, L.E., "Time History Effects on a Rolling 65 Deg Delta-Wing-Body Configuration," Paper 97-3645, AIAA Atmospheric Flight Mechanics Conference, August 1997, New Orleans, LA.
    • (1997) AIAA Atmospheric Flight Mechanics Conference
    • Ericsson, L.E.1
  • 10
    • 84983097761 scopus 로고    scopus 로고
    • Multiple Time-Scale Effects for a Pitching 65° Delta Wing
    • Paper 98-4354, August, Boston MA
    • Myatt, J.H., "Multiple Time-Scale Effects for a Pitching 65° Delta Wing," Paper 98-4354, AIAA Atmosperic Flight Mechanics Conference, August 1998, Boston MA.
    • (1998) AIAA Atmosperic Flight Mechanics Conference
    • Myatt, J.H.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.