Flight Dynamics Publications

For clarity, the list of publications below is approximately grouped according to subject category. Some of the papers, for which the author has the copyright, are available for download in the column to the right.

Robust Flutter Solution Methods

D. Borglund and U. Ringertz. Solution of the Flutter Eigenvalue Problem with Mixed Structural/Aerodynamic Uncertainty. Journal of Aircraft 48(1):343-348, January 2011. doi: 10.2514/1.C031204

D. Borglund and U. Ringertz. Solution of the uncertain flutter eigenvalue problem using the μ-p method. International Forum on Aeroelasticity and Structural Dynamics, Seattle, June 2009. Paper IFASD-2009-048.

S. Heinze and U. Ringertz and D. Borglund. Assessment of Uncertain External Store Aerodynamics Using μ-p Flutter Analysis. Journal of Aircraft, 46(3):1062-1068, May 2009, doi: 10.2514/1.39158

S. Heinze and D. Borglund. Robust Flutter Analysis Considering Mode Shape Variations. Journal of Aircraft, 45(3):1070-1075, May 2008, doi: 10.2514/1.28728

D. Borglund. Robust Eigenvalue Analysis Using the Structured Singular Value: The µ-p Flutter Method, AIAA Journal, 46(11):2806-2813, November 2008, doi: 10.2514/1.35859

D. Borglund. Robust Aeroelastic Analysis in the Laplace Domain: The μ-p Method. International Forum on Aeroelasticity and Structural Dynamics, Stockholm, June 2007. Paper IFASD-2007-011.

S. Heinze and U. Ringertz and D. Borglund. On Uncertainty Modeling and Validation for External Store Aerodynamics. International Forum on Aeroelasticity and Structural Dynamics, Stockholm, June 2007. Paper IFASD-2007-040.

S. Heinze. Assessment of Critical Fuel Configurations Using Robust Flutter Analysis. Journal of Aircraft, 44(6):2034-2039, November 2007, doi: 10.2514/1.30500

D. Borglund. Efficient Computation of Robust Flutter Boundaries Using the μ-k Method. Journal of Aircraft 43(6):1763-1769, November 2006, doi: 10.2514/1.20190

D. Borglund. Upper Bound Flutter Speed Estimation Using the μ-k Method. Journal of Aircraft, 42(2):555-557, January 2002, doi: 10.2514/1.7586

D. Borglund. The μ-k Method for Robust Flutter Solutions. Journal of Aircraft, 41(5):1209-1216, September 2004, doi: 10.2514/1.3062

D. Borglund and U. Nilsson. Robust Wing Flutter Suppression Considering Aerodynamic Uncertainty. Journal of Aircraft, 41(2):331-334, March 2004, doi: 10.2514/1.9328

D. Borglund. Robust Aeroelastic Stability Analysis Considering Frequency-Domain Aerodynamic Uncertainty. Journal of Aircraft, 40(1):189-193, January 2003, doi: 10.2514/2.3074

J. Kuttenkeuler. A Finite Element Based Modal Method for Determination of Plate Stiffnesses Considering Uncertainties. Journal of Composite Materials, 33:695-711, 1999.

Experimental Aeroelasticity

G. Stenfeldt, U. Ringertz. Yaw Control of a Tailless Aircraft Configuration. Journal of Aircraft 47(5):1807-1810, September 2010, doi: 10.2514/1.C031017

G. Stenfelt, U. Ringertz. Lateral Stability and Control of a Tailless Aircraft Configuration. Journal of Aircraft 46(6):2161-2164, November 2009, doi: 10.2514/1.41092

S. Heinze and M. Karpel. Analysis and Wind Tunnel Testing of a Piezoelectric Tab for Aeroelastic Control Applications. Journal of Aircraft, 43(6):1799-1804, November 2006, doi: 10.2514/1.20060

M. Carlsson. Control Surface Response of a Blended Wing Body Aeroelastic Wind Tunnel Model. Journal of Aircraft, 42(3):738-742, 2005, doi: 10.2514/1.5440

M. Carlsson and C. Cronander. Efficient roll control using distributed control surfaces and aeroelastic effects. Aerospace Science & Technology, 9(2):143-150, 2005

M. Carlsson. Aeroelastic Model Design Using an Integrated Optimization Approach. Journal of Aircraft, 41(6):1523-1529, 2005, doi: 10.2514/1.8431

M. Carlsson and J. Kuttenkeuler. Design and Testing of a Blended Wing Body Aeroelastic Wind Tunnel Model. Journal of Aircraft, 40(1):211-213, 2003

D. Borglund and I. M. Kroo. Aeroelastic Design Optimization of a Two-Spar Flexible Wind-Tunnel Model. Journal of Aircraft, 39(6):1074-1076, 2002, doi: 10.2514/2.3038

D. Borglund and J. Kuttenkeuler. Active wing flutter suppression using a trailing edge flap. Journal of Fluids and Structures, 16(3):271-294, 2002.

D. Borglund. Aeroservoelastic design optimization with experimental verification. Journal of Aircraft, 38(5):958-961, 2001.

J. Kuttenkeuler. Optical Measurements of Flutter Mode Shapes. Journal of Aircraft, 37(5):846-849, 2000.

C. Cronander and U. Ringertz. Closed loop roll control using aeroelastic information. Aerospace Science and Technology, 4:481-494, 2000.

D. Borglund. Active nozzle control and integrated design optimization of a beam subject to fluid-dynamic forces. Journal of Fluids and Structures 13(2):269-287, 1999.

M. H. Fredriksson, D. Borglund and A. B. Nordmark. Experiments on the onset of impacting motion using a pipe conveying fluid. Nonlinear Dynamics, 19:261-271, 1999.

J. Kuttenkeuler and U. Ringertz. Aeroelastic design optimization with experimental verification. Journal of Aircraft, 35:505-507, 1998.

D. Borglund. On the optimal design of pipes conveying fluids. Journal of Fluids and Structures 12(3):353-365, 1998.

Trajectory Optimization and Green Operations

M. Jacobsen and U. Ringertz. Airspace Constraints in Aircraft Emission Trajectory Optimization. Journal of Aircraft 47(4):1256-1265, July 2010, doi: 10.2514/1.47109

M. Jacobsen and U. Ringertz. Performance optimization of flexible wings using multiple control surfaces. International Forum on Aeroelasticity and Structural Dynamics, Seattle, June 2009. Paper IFASD-2009-003.

M. Jacobsen. Real time drag minimization using redundant control surfaces.
Aerospace Science & Technology, 10(7):574-580, October 2006

M. Norsell. Multistage Trajectory Optimization with Radar Range Constraints.
Journal of Aircraft, 42(4):849-857, 2005, doi: 10.2514/1.8544

M. Norsell. Radar cross section constraints in flight-path optimization.
Journal of Aircraft, 40(2):412-415, 2003

M. Norsell. Aircraft trajectories considering radar range constraints.
Aerospace Science & Technology, 6:83-89, 2002.

M. Norsell. Flight testing radar detection of the Saab 105 in level flight.
AIAA Journal of Aircraft, 39(5):894-897, 2002.

U. Ringertz. An optimal trajectory for a minimum fuel turn. Journal of Aircraft, 37(5):932-934, 2000.

U. Ringertz. Flight testing an optimal trajectory for the Saab J35 Draken. Journal of Aircraft, 37(1):187-189, 2000.

Teaching and Learning

D. Borglund. A case study of peer learning in higher aeronautical education. European Journal of Engineering Education, 32(1):35-42, 2007.

Computational Methods in Aeroelasticity

N. Jansson and D. Eller. Robust Turbulence Load Alleviation. International Forum on Aeroelasticity and Structural Dynamics, Paris, June 2011. Paper IFASD-2011-144.

D. Eller. Non-iterative solution of the flutter eigenvalue problem using Laplace-domain aerodynamic loads. International Forum on Aeroelasticity and Structural Dynamics, Seattle, June 2009. Paper IFASD-2009-119.

M. Tomac and D.Eller. From Geometry to CFD-Based Aerodynamic Derivatives - An Automated Approach. 27th International Congress of the Aeronautical Sciences, September 2010, Nice, France.

D. Eller. Flutter Equation as a Piecewise Quadratic Eigenvalue Problem. Journal of Aircraft, 46(3):1068-1070, May 2009, doi: 10.2514/1.40653

D. Eller. Friction, Freeplay and Flutter of Manually Controlled Aircraft. International Forum on Aeroelasticity and Structural Dynamics, Stockholm, June 2007.

D. Eller and S. Heinze. An Approach to Induced Drag Reduction with Experimental Evaluation. Journal of Aircraft, 42(6):1478-1485, November 2005.

D. Eller. Efficient Flight Mechanics Simulation of Elastic Aircraft Configurations. International Forum for Aeroelasticity and Structural Dynamics, Munich, June 2005.

D. Eller and M. Carlsson. An Efficient Aerodynamic Boundary Element Method for Aeroelastic Simulations and its Experimental Validation. Aerospace Science & Technology, 7(7):532-539, 2003

D. Berggren. Experimental validation of nonlinear shell structural dynamics. AIAA Journal, 9:1825-1827, 2001.

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