-
1
-
-
7544220667
-
cent results and research challenges
-
doi:10.2514/1.3961
-
Pettit, C., "Uncertainty Quantification in Aeroelasticity: Recent Results and Research Challenges," Journal of Aircraft, Vol. 41, No. 5, 2004, pp. 1217-1229. doi:10.2514/1.3961
-
(2004)
Journal of Aircraft
, vol.41
, Issue.5
, pp. 1217-1229
-
-
Pettit, C.1
-
2
-
-
0003585352
-
-
Prentice-Hall Upper Saddle River NJ, Chap. 11
-
Zhou, K., Doyle, J. C., and Glover, K., Robust and Optimal Control, Prentice-Hall, Upper Saddle River, NJ, 1996, Chap. 11.
-
(1996)
Robust and Optimal Control
-
-
Zhou, K.1
Doyle, J.C.2
Glover, K.3
-
4
-
-
0036178635
-
Match-point solutions for robust flutter analysis
-
Lind, R., "Match-Point Solutions for Robust Flutter Analysis," Journal of Aircraft, Vol. 39, No. 1, 2002, pp. 91-99. doi:10.2514/2.2900 (Pubitemid 34172798)
-
(2002)
Journal of Aircraft
, vol.39
, Issue.1
, pp. 91-99
-
-
Lind, R.1
-
5
-
-
0028604153
-
An approach to modelvalidation in the μ framework
-
Baltimore MD IEEE Publ., Piscataway, NJ
-
Kumar, A., and Balas, G. J., "An Approach to ModelValidation in the μ Framework," Proceedings of the American Control Conference, Baltimore, MD, IEEE Publ., Piscataway, NJ, 1994, pp. 3021-3026.
-
(1994)
Proceedings of the American Control Conference
, pp. 3021-3026
-
-
Kumar, A.1
Balas, G.J.2
-
6
-
-
0034314729
-
Flutterometer: An on-line tool to predict robust flutter margins
-
Lind, R., and Brenner, M., "Flutterometer: An On-Line Tool to Predict Robust Flutter Margins," Journal of Aircraft, Vol. 37, No. 6, 2000, pp. 1105-1112. doi:10.2514/2.2719 (Pubitemid 32089603)
-
(2000)
Journal of Aircraft
, vol.37
, Issue.6
, pp. 1105-1112
-
-
Lind, R.1
Brenner, M.2
-
7
-
-
0036640838
-
Aeroservoelastic model uncertainty bound estimation from flight data
-
Brenner, M., "Aeroservoelastic Model Uncertainty Bound Estimation from Flight Data," Journal of Guidance, Control, and Dynamics, Vol. 25, No. 4, 2002, pp. 748-754. doi:10.2514/2.4942 (Pubitemid 34799844)
-
(2002)
Journal of Guidance, Control, and Dynamics
, vol.25
, Issue.4
, pp. 748-754
-
-
Brenner, M.J.1
-
8
-
-
7544234974
-
The-k method for robust flutter solutions
-
doi:10.2514/1.3062
-
Borglund, D., "The-k Method for Robust Flutter Solutions," Journal of Aircraft, Vol. 41, No. 5, 2004, pp. 1209-1216. doi:10.2514/1.3062
-
(2004)
Journal of Aircraft
, vol.41
, Issue.5
, pp. 1209-1216
-
-
Borglund, D.1
-
9
-
-
33846046340
-
Efficient computation of robust flutter boundaries using the μ-k method
-
DOI 10.2514/1.20190
-
Borglund, D., and Ringertz, U., "Efficient Computation of Robust Flutter Boundaries Using the μ-k Method," Journal of Aircraft,Vol. 43, No. 6, 2006, pp. 1763-1769. doi:10.2514/1.20190 (Pubitemid 46065241)
-
(2006)
Journal of Aircraft
, vol.43
, Issue.6
, pp. 1763-1769
-
-
Borglund, D.1
Ringertz, U.2
-
10
-
-
18144416970
-
Upper-bound flutter speed estimation using the μ-k method
-
Borglund, D., "Upper-Bound Flutter Speed Estimation Using the μ-k Method," Journal of Aircraft, Vol. 42, No. 2, 2005, pp. 555-557. doi:10.2514/1.7586 (Pubitemid 40611756)
-
(2005)
Journal of Aircraft
, vol.42
, Issue.2
, pp. 555-557
-
-
Borglund, D.1
-
11
-
-
55749090977
-
Robust eigenvalue analysis using the structured singular value: The-p flutter method
-
doi:10.2514/1.35859
-
Borglund, D., "Robust Eigenvalue Analysis Using the Structured Singular Value: The-p Flutter Method," AIAA Journal, Vol. 46, No. 11, 2008, pp. 2806-2813. doi:10.2514/1.35859
-
(2008)
AIAA Journal
, vol.46
, Issue.11
, pp. 2806-2813
-
-
Borglund, D.1
-
12
-
-
79551679483
-
Robust aeroelastic analysis of the gripen fighter including flight test model validation
-
Paper IF-019, Stockholm, Sweden
-
Carlsson, M., and Karlsson, A., "Robust Aeroelastic Analysis of the Gripen Fighter Including Flight Test Model Validation," CEAS/AIAA/KTH International Forum on Aeroelasticity and Structural Dynamics, Paper IF-019, Stockholm, Sweden, 2007.
-
(2007)
CEAS/AIAA/KTH International Forum on Aeroelasticity and Structural Dynamics
-
-
Carlsson, M.1
Karlsson, A.2
-
13
-
-
0000039343
-
Convergence of methods for nonlinear eigenvalue problems
-
Bäck, P., and Ringertz, U. T., "Convergence of Methods for Nonlinear Eigenvalue Problems," AIAA Journal, Vol. 35, No. 6, 1997, pp. 1084-1087. doi:10.2514/2.200 (Pubitemid 127563373)
-
(1997)
AIAA Journal
, vol.35
, Issue.6
, pp. 1084-1087
-
-
Back, P.1
Ringertz, U.2
-
14
-
-
0034276174
-
Damping perturbation method for flutter solution: The g-method
-
doi:10.2514/2.1171
-
Chen, P. C., "Damping Perturbation Method for Flutter Solution: The g-Method," AIAA Journal, Vol. 38, No. 9, 2000, pp. 1519-1524. doi:10.2514/2.1171
-
(2000)
AIAA Journal
, vol.38
, Issue.9
, pp. 1519-1524
-
-
Chen, P.C.1
-
15
-
-
38149030900
-
Assessment of critical fuel configurations using robust flutter analysis
-
doi:10.2514/1.30500
-
Heinze, S., "Assessment of Critical Fuel Configurations Using Robust Flutter Analysis," Journal of Aircraft, Vol. 44, No. 6, 2007, pp. 2034-2039. doi:10.2514/1.30500
-
(2007)
Journal of Aircraft
, vol.44
, Issue.6
, pp. 2034-2039
-
-
Heinze, S.1
-
16
-
-
79961062587
-
Solution of the uncertain flutter eigenvalue problem using the μ-p method
-
IFASD Paper 2009-048, Seattle, WA
-
Borglund, D., and Ringertz, U., "Solution of the Uncertain Flutter Eigenvalue Problem Using the μ-p Method," CEAS/AIAA International Forum on Aeroelasticity and Structural Dynamics, IFASD Paper 2009-048, Seattle, WA, 2009.
-
(2009)
CEAS/AIAA International Forum on Aeroelasticity and Structural Dynamics
-
-
Borglund, D.1
Ringertz, U.2
-
17
-
-
79961083804
-
-
International Council of the Aeronautical Sciences Paper 90-1.2.3, Bonn, Germany
-
Stark, V. J., "The AEREL Flutter Prediction System," International Council of the Aeronautical Sciences Paper 90-1.2.3, Bonn, Germany, 1990.
-
(1990)
The AEREL Flutter Prediction System
-
-
Stark, V.J.1
-
18
-
-
84907338174
-
Influence of nonplanar supersonic interference on aeroelastic characteristics
-
Williamsburg, VA, NASA CP 1999-209136/PT1
-
Kouzmin, V., Kouzmin, S., Mosounov, V., and Ishmuratov, F., "Influence of Nonplanar Supersonic Interference on Aeroelastic Characteristics," CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics, Williamsburg, VA, NASA CP 1999-209136/PT1, 1999, pp. 415-424.
-
(1999)
CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics
, pp. 415-424
-
-
Kouzmin, V.1
Kouzmin, S.2
Mosounov, V.3
Ishmuratov, F.4
-
19
-
-
67650882495
-
Assessment of uncertain external store aerodynamics using μ-p flutter analysis
-
doi:10.2514/1.39158
-
Heinze, S., Ringertz, U., and Borglund, D., "Assessment of Uncertain External Store Aerodynamics Using μ-p Flutter Analysis," Journal of Aircraft, Vol. 46, No. 3, 2009, pp. 1062-1067. doi:10.2514/1.39158
-
(2009)
Journal of Aircraft
, vol.46
, Issue.3
, pp. 1062-1067
-
-
Heinze, S.1
Ringertz, U.2
Borglund, D.3
-
20
-
-
79961058970
-
Flutter testing methods at saab military aircraft
-
Lancaster, CA
-
Olert, L., and Karlsson, T., "Flutter Testing Methods at Saab Military Aircraft," 7th European Chapter Symposium, Amsterdam, Soc. of Flight Test Engineers Paper A1994-12, Lancaster, CA, 1994.
-
(1994)
7th European Chapter Symposium, Amsterdam, Soc. of Flight Test Engineers Paper A1994-12
-
-
Olert, L.1
Karlsson, T.2
-
21
-
-
0003426684
-
-
Kluwer Academic, Norwell, MA, 131
-
Van Overschee, P., and De Moor, B., Subspace Identification for Linear Systems, Kluwer Academic, Norwell, MA, 1996, pp. 90, 131.
-
(1996)
Subspace Identification for Linear Systems
, pp. 90
-
-
Van Overschee, P.1
De Moor, B.2
|