logging in or signing up Aeroelastic ozturk Download Post to : URL : Related Presentations : Share Add to Flag Embed Email Send to Blogs and Networks Add to Channel Uploaded from authorPOINTLite Insert YouTube videos in PowerPont slides with aS Desktop Copy embed code: (To copy code, click on the text box) Embed: URL: Thumbnail: WordPress Embed Customize Embed The presentation is successfully added In Your Favorites. Views: 856 Category: Education License: All Rights Reserved Like it (0) Dislike it (0) Added: January 04, 2008 This Presentation is Public Favorites: 0 Presentation Description No description available. Comments Posting comment... Premium member Presentation Transcript Aeroelastic effects: Aeroelastic effects Wind loading and structural response Lecture 14 Dr. J.D. HolmesAeroelastic effects: Aeroelastic effects Very flexible dynamically wind-sensitive structures Motion of the structure generates aerodynamic forces Positive aerodynamic damping : reduces vibrations - steel lattice towers if forces act in direction to increase the motion : aerodynamic instabilityAeroelastic effects: Aeroelastic effects Example : Tacoma Narrows Bridge WA - 1940 Example : ‘Galloping’ of iced-up transmission linesAeroelastic effects: Aeroelastic effects Aerodynamic damping (along wind) : Aeroelastic effects: Aeroelastic effects Aerodynamic damping (along wind) : Drag force (per unit length) = along-wind aerodynamic damping is positiveAeroelastic effects: Aeroelastic effects Galloping : galloping is a form of aerodynamic instability caused by negative aerodynamic damping in the cross wind direction Motion of body in z direction will generate an apparent reduction in angle of attack, Aeroelastic effects: Aeroelastic effects Galloping : Aerodynamic force per unit length in z direction (body axes) : (Lecture 8) For = 0 : Aeroelastic effects: Aeroelastic effects Galloping : negative aerodynamic damping when transposed to left-hand sideAeroelastic effects: Aeroelastic effects Galloping : den Hartog’s Criterion critical wind speed for galloping,Ucrit , occurs when total damping is zero Since c = 2(mk)=4mn1 (Figure 5.5 in book) m = mass per unit length n1 = first mode natural frequencyAeroelastic effects: Galloping : Cross sections prone to galloping : Square section (zero angle of attack) D-shaped cross section iced-up transmission line or guy cable Aeroelastic effectsAeroelastic effects: Aeroelastic effects Flutter : Can generate a cross-wind force and a moment Aerodynamic instabilities involving rotation are called ‘flutter’Aeroelastic effects: Aeroelastic effects Flutter : General equations of motion for body free to rotate and translate : per unit mass per unit mass moment of inertiaAeroelastic effects: Aeroelastic effects Flutter : Types of instabilities :Aeroelastic effects: Flutter : Flutter derivatives for two bridge deck sections : Aeroelastic effectsAeroelastic effects: Aeroelastic effects Flutter : Determination of critical flutter speed for long-span bridges: Empirical formula (e.g. Selberg) Experimental determination (wind-tunnel model) Theoretical analysis using flutter derivatives obtained experimentallyAeroelastic effects: Aeroelastic effects Lock - in : Motion-induced forces during vibration caused by vortex shedding Frequency ‘locks-in’ to frequency of vibration Strength of forces and correlation length increased End of Lecture 14John Holmes225-405-3789 JHolmes@lsu.edu: End of Lecture 14 John Holmes 225-405-3789 JHolmes@lsu.edu You do not have the permission to view this presentation. In order to view it, please contact the author of the presentation.
Aeroelastic ozturk Download Post to : URL : Related Presentations : Share Add to Flag Embed Email Send to Blogs and Networks Add to Channel Uploaded from authorPOINTLite Insert YouTube videos in PowerPont slides with aS Desktop Copy embed code: (To copy code, click on the text box) Embed: URL: Thumbnail: WordPress Embed Customize Embed The presentation is successfully added In Your Favorites. Views: 856 Category: Education License: All Rights Reserved Like it (0) Dislike it (0) Added: January 04, 2008 This Presentation is Public Favorites: 0 Presentation Description No description available. Comments Posting comment... Premium member Presentation Transcript Aeroelastic effects: Aeroelastic effects Wind loading and structural response Lecture 14 Dr. J.D. HolmesAeroelastic effects: Aeroelastic effects Very flexible dynamically wind-sensitive structures Motion of the structure generates aerodynamic forces Positive aerodynamic damping : reduces vibrations - steel lattice towers if forces act in direction to increase the motion : aerodynamic instabilityAeroelastic effects: Aeroelastic effects Example : Tacoma Narrows Bridge WA - 1940 Example : ‘Galloping’ of iced-up transmission linesAeroelastic effects: Aeroelastic effects Aerodynamic damping (along wind) : Aeroelastic effects: Aeroelastic effects Aerodynamic damping (along wind) : Drag force (per unit length) = along-wind aerodynamic damping is positiveAeroelastic effects: Aeroelastic effects Galloping : galloping is a form of aerodynamic instability caused by negative aerodynamic damping in the cross wind direction Motion of body in z direction will generate an apparent reduction in angle of attack, Aeroelastic effects: Aeroelastic effects Galloping : Aerodynamic force per unit length in z direction (body axes) : (Lecture 8) For = 0 : Aeroelastic effects: Aeroelastic effects Galloping : negative aerodynamic damping when transposed to left-hand sideAeroelastic effects: Aeroelastic effects Galloping : den Hartog’s Criterion critical wind speed for galloping,Ucrit , occurs when total damping is zero Since c = 2(mk)=4mn1 (Figure 5.5 in book) m = mass per unit length n1 = first mode natural frequencyAeroelastic effects: Galloping : Cross sections prone to galloping : Square section (zero angle of attack) D-shaped cross section iced-up transmission line or guy cable Aeroelastic effectsAeroelastic effects: Aeroelastic effects Flutter : Can generate a cross-wind force and a moment Aerodynamic instabilities involving rotation are called ‘flutter’Aeroelastic effects: Aeroelastic effects Flutter : General equations of motion for body free to rotate and translate : per unit mass per unit mass moment of inertiaAeroelastic effects: Aeroelastic effects Flutter : Types of instabilities :Aeroelastic effects: Flutter : Flutter derivatives for two bridge deck sections : Aeroelastic effectsAeroelastic effects: Aeroelastic effects Flutter : Determination of critical flutter speed for long-span bridges: Empirical formula (e.g. Selberg) Experimental determination (wind-tunnel model) Theoretical analysis using flutter derivatives obtained experimentallyAeroelastic effects: Aeroelastic effects Lock - in : Motion-induced forces during vibration caused by vortex shedding Frequency ‘locks-in’ to frequency of vibration Strength of forces and correlation length increased End of Lecture 14John Holmes225-405-3789 JHolmes@lsu.edu: End of Lecture 14 John Holmes 225-405-3789 JHolmes@lsu.edu