1-24 of 30 Books
X-38 vehicle 131 flutter assessment
X-38 vehicle 131 flutter assessment
By James P. Smith - undifferentiated
Nonlinear aspects of transonic aeroelasticity
Nonlinear aspects of transonic aeroelasticity
By Hema Sandhyarani Murty
Application of TURBO-AE to flutter prediction
Application of TURBO-AE to flutter prediction
By Daniel Hoyniak
A worst-case approach for on-line flutter prediction
A worst-case approach for on-line flutter prediction
By Rick C. Lind
Methods for in-flight robustness evaluation
Methods for in-flight robustness evaluation
By James D. Paduano
FPCAS3D user's guide
FPCAS3D user's guide
By Milind A. Bakhle
Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments
Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments
By Robert V. Doggett
Advanced aeroservoelastic testing and data analysis
Advanced aeroservoelastic testing and data analysis
By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.
Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model
Using transonic small disturbance theory for predicting the aeroelastic stability of a flexible wind-tunnel model
By Walter A. Silva
CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999
CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999
By CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics (1999 Williamsburg, Va.)
Transonic flutter analysis using the Euler equations
Transonic flutter analysis using the Euler equations
By Oddvar O. Bendiksen
Developing uncertainty models for robust flutter analysis using ground vibration test data
Developing uncertainty models for robust flutter analysis using ground vibration test data
By Starr Potter
Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I
Flutter clearance of the F-14 variable-sweep transition flight experiment airplane, phase I
By M. W. Kehoe
Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
Experimental and analytical investigation of the effect of spanwise curvature on wing flutter at Mach number of 0.7
By Jose A. Rivera
A presentation on robust flutter margin analysis and a flutterometer
A presentation on robust flutter margin analysis and a flutterometer
By Rick C. Lind
Control surface spanwise placement in active flutter suppresssion systems
Control surface spanwise placement in active flutter suppresssion systems
By E. Nissim
Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances
Flow visualization study of a 1/48-scale AFTI/F111 model to investigate horizontal tail flow disturbances
By Lisa J. Bjarke
Optimization of training sets for neural-net processing of characteristic patterns from vibrating solids
Optimization of training sets for neural-net processing of characteristic patterns from vibrating solids
By Arthur J. Decker
Analytical study of helicopter rotor blade stall flutter charcteristics
Analytical study of helicopter rotor blade stall flutter charcteristics
By L. M. Casellini
An interactive software for conceptual wing flutter analysis and parametric study
An interactive software for conceptual wing flutter analysis and parametric study
By Vivek Mukhopadhyay
Mass balancing of hollow fan blades
Mass balancing of hollow fan blades
By Robert E. Kielb
Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver
Flutter and forced response analyses of cascades using a two-dimensional linearized Euler solver
By T. S. R. Reddy
Modern wing flutter analysis by computational fluid dynamics methods
Modern wing flutter analysis by computational fluid dynamics methods
By Herbert J. Cunningham
Flutter analysis of a two-dimensional airfoil with cubic non-linear restoring force
Flutter analysis of a two-dimensional airfoil with cubic non-linear restoring force
By B. H. K. Lee