Explore Books on
flutter
1-24 of 56 Books
In-flight investigation of a rotating cylinder-based structural excitation system for flutter testing
In-flight investigation of a rotating cylinder-based structural excitation system for flutter testing
By Lura Vernon
Evaluation of diffuse-illumination holographic cinematography in a flutter cascade
Evaluation of diffuse-illumination holographic cinematography in a flutter cascade
By Arthur J. Decker
Flutter of a low-aspect-ratio rectangular wing
Flutter of a low-aspect-ratio rectangular wing
By Stanley R. Cole
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
Correlation filtering of modal dynamics using the Laplace wavelet
Correlation filtering of modal dynamics using the Laplace wavelet
By Lawrence C. Freudinger
Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
By Osama A. Kandil
Improved flight test procedures for flutter clearance
Improved flight test procedures for flutter clearance
By Rick C. Lind
Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
By Lawrence C. Freudinger
Flow limitation and flutter in membrane walled collapsible tubes: a model for expiratory wheezing
Flow limitation and flutter in membrane walled collapsible tubes: a model for expiratory wheezing
By Colin Walsh
Overview of recent flight flutter testing research at NASA Dryden
Overview of recent flight flutter testing research at NASA Dryden
By Martin J. Brenner
Ground vibration test of an F-16 airplane with modified decoupler pylons
Ground vibration test of an F-16 airplane with modified decoupler pylons
By F. W. Cazier
Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model
Effects of winglet on transonic flutter characteristics of a cantilevered twin-engine-transport wing model
By Charles L. Ruhlin
Research and applications in structures at the NASA Langley Research Center
Research and applications in structures at the NASA Langley Research Center
By Irving Abel
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
Planform curvature effects on flutter characteristics of a wing with 56 degree leading-edge sweep and panel aspect ratio of 1.14
Planform curvature effects on flutter characteristics of a wing with 56 degree leading-edge sweep and panel aspect ratio of 1.14
By Donald F. Keller
Final technical report for aeroelastic analysis of turbomachinery for space propulsion
Final technical report for aeroelastic analysis of turbomachinery for space propulsion
By Theo G. Keith
ASTROP2 users manual
ASTROP2 users manual
By T. S. R. Reddy
Aeroelastic calculations using CFD for a typical business jet model
Aeroelastic calculations using CFD for a typical business jet model
By Michael D. Gibbons
The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis
The Green's function method for fully unsteady aerodynamics around three-dimensional bodies and its application to flutter analysis
By Qiangang Liu
Bibliography of vibration and flutter of aircraft wings and control surfaces
Bibliography of vibration and flutter of aircraft wings and control surfaces
By Alexander Klemin
Preliminary investigation of the air loads on an oscillating two-dimensional aerofoil with leading and trailing edge flap, with emphasis on the negative stall
Preliminary investigation of the air loads on an oscillating two-dimensional aerofoil with leading and trailing edge flap, with emphasis on the negative stall
By D. R. Madill