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Volumn , Issue , 2003, Pages

Validation of methodology for estimating aircraft unsteady aerodynamic parameters from dynamic wind tunnel tests

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODELING; DYNAMIC WIND TUNNEL TESTS; FORCED OSCILLATIONS; IN-FLIGHT DYNAMICS; INDICIAL FUNCTIONS; MATHEMATICAL FORMULATION; NONLINEAR UNSTEADY AERODYNAMICS; UNSTEADY AERODYNAMICS;

EID: 84896693121     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (24)

References (9)
  • 3
    • 84896848544 scopus 로고    scopus 로고
    • Eidetics Corporation: Final Report; SBIR Phase II Final Report, Naval Air Warfare Center Aircraft Division, TR00-002, June 11
    • Eidetics Corporation: Final Report; Determination of Nonlinear Dynamic Aerodynamic Coefficients for Aircraft, SBIR Phase II Final Report, Naval Air Warfare Center Aircraft Division, TR00-002, June 11, 2000.
    • (2000) Determination of Nonlinear Dynamic Aerodynamic Coefficients For Aircraft
  • 6
    • 0028498390 scopus 로고
    • State-Space Representation of Aerodynamic Characteristics at High Angles of Attack
    • Sept.-Oct
    • Goman, M. and Khrabrov, A.: State-Space Representation of Aerodynamic Characteristics 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.1    Khrabrov, A.2
  • 8
    • 0014710684 scopus 로고
    • Synthesis of Low-Peak-Factor Signals and Binary Sequences with Low Autocorrelation
    • January
    • Schroeder, M.R.: Synthesis of Low-Peak-Factor Signals and Binary Sequences with Low Autocorrelation, IEEE Transactions on Information Theory, January 1970, pp. 85-89.
    • (1970) IEEE Transactions On Information Theory , pp. 85-89
    • Schroeder, M.R.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.