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Journal of Aircraft

Volumn 38, Issue 4, 2001, Pages 755-763

Accurate subcritical damping solution of flutter equation using piecewise aerodynamic function

(1) Goodman, C a

a BOEING COMPANY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DAMPING; EIGENVALUES AND EIGENFUNCTIONS; INTERPOLATION; MATHEMATICAL MODELS; PIECEWISE LINEAR TECHNIQUES; STATE SPACE METHODS;

PIECEWISE AERODYNAMIC FUNCTION; SUBCRITICAL DAMPING;

FLUTTER (AERODYNAMICS);

EID: 0035390401 PISSN: 00218669 EISSN: 15333868 Source Type: Journal
DOI: 10.2514/2.2828 Document Type: Article

Times cited : (14)

References (7)

1
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2
- 0015160179
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- Hassig, H.J.¹

3
- 85037410664
- Improved curve fitting techniques of frequency domain generalized aerodynamic forces
- AIAA Paper 88-4355-CP, AIAA, Washington, DC
- (1990) 31st Structures, Structural Dynamics and Materials Conference , pp. 233-243
- Sallee, V.J.¹

4
- 0005857424
- FAMUSS: A new aeroservoelastic modeling tool
- AIAA, Washington, DC
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5
- 0004320199
- AIAA Paper 98-1897, April
- (1998) Reduced Order Dynamic Aeroelastic Model Development and Integration with Nonlinear Simulation
- Winther, B.A.¹ Goggin, P.J.² Dykman, J.R.³

6
- 0003814628
- Air Force Flight Dynamics Lab. Rept. AFFDL-TR-71-5, Wright-Patterson AFB, Dayton, OH, Nov.
- (1971) Subsonic Unsteady Aerodynamics for General Configurations
- Giesing, J.P.¹ Kalman, T.P.² Rodden, W.P.³

7
- 0004356489
- NASA-TP-2292, March
- (1984) Generalization of the Subsonic Kernel Function in the s-Plane, with Applications to Flutter Analysis
- Cunningham, H.J.¹ Desmarais, R.N.²

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.