000 04475nam a22003735i 4500
001 287463
003 MX-SnUAN
005 20160429154548.0
007 cr nn 008mamaa
008 150903s2011 xxu| o |||| 0|eng d
020 _a9781441993021
_99781441993021
024 7 _a10.1007/9781441993021
_2doi
035 _avtls000339279
039 9 _a201509030837
_bVLOAD
_c201404300357
_dVLOAD
_y201402060931
_zstaff
040 _aMX-SnUAN
_bspa
_cMX-SnUAN
_erda
050 4 _aTL787-4050.22
100 1 _aProulx, Tom.
_eeditor.
_9315871
245 1 0 _aAdvanced Aerospace Applications, Volume 1 :
_bProceedings of the 29th IMAC, A Conference on Structural Dynamics, 2011 /
_cedited by Tom Proulx.
264 1 _aNew York, NY :
_bSpringer New York :
_bImprint: Springer,
_c2011.
300 _aIx, 368 páginas
_brecurso en línea.
336 _atexto
_btxt
_2rdacontent
337 _acomputadora
_bc
_2rdamedia
338 _arecurso en línea
_bcr
_2rdacarrier
347 _aarchivo de texto
_bPDF
_2rda
490 0 _aConference Proceedings of the Society for Experimental Mechanics Series,
_x2191-5644
500 _aSpringer eBooks
505 0 _aHigh Frequency Optimisation of an Aerospace Structure Through Sensitivity to SEA Parameters -- Converting a Driven Base Vibration Test to a Fixed Base Modal Analysis -- Advanced Operational Modal Analysis Methods for Linear Time Periodic System Identification -- Benefit of Acoustic Particle Velocity Based Reverberant Room Testing of Space Structures -- Ultrasonic Vibration Modal Analysis Technique (UMAT) for Defect Detection -- Acoustic Testing and Response Prediction of the CASSIOPE Spacecraft -- Force Limited Vibration Testing Applied to the JWST FGS OA -- On Force Limited Vibration for Testing Space Hardware -- Calculation of Rigid Body Mass Properties of Flexible Structures -- Simulating Base-shake Environmental Testing -- Geometry-based Updating of 3D Solid Finite Element Models -- A PZT-based Technique for SHM Using the Coherence Function -- The Best Force Design of Pure Modal Test Based Upon a Singular Value Decomposition Approach -- Modal Identification and Model Updating of Pleiades -- Aircraft GVT Advances and Application – Gulfstream G650 -- Aircraft Dynamics and Payload Interaction – SOFIA Telescope -- Application of Modal Analysis for Evaluation of the Impact Resistance of Aerospace Sandwich Materials -- An Integrated Procedure for Estimating Modal Parameters During Flight Testing -- Multiple-site Damage Location Using Single-site Training Data -- "Assessment of Nonlinear System Identification Methods Using the -- SmallSat Spacecraft Structure" -- Ground Vibration Testing Master Class: Modern Testing and Analysis Concepts Applied to an F-16 Aircraft -- Advanced Shaker Excitation Signals for Aerospace Testing -- System and Method for Compensating Structural Vibrations of an Aircraft Caused by Outside Disturbances -- Operational Modal Analysis on a Modified Helicopter -- Development of New Discrete Wavelet Families for Structural Dynamic Analysis -- Model Updating With Neural Networks and Genetic Optimization -- A Piezoelectric Actuated Stabilization Mount for Payloads Onboard Small UAS -- Extraction of Modal Parameters From Spacecraft Flight Data -- Dynamic Characterization of Satellite Components Through Non-invasive Methods -- An Inertially Referenced Non-contact Sensor for Ground Vibration Tests -- Reliability of Experimental Modal Data Determined on Large Spaceflight Structures -- Operational Modal Analysis of a Spacecraft Vibration Test.-.
520 _aAdvanced Aerospace Applications, Volume 1. Proceedings of the 29th IMAC, A Conference and Exposition on Structural Dynamics, 2011, the first volume of six from the Conference, brings together 32 contributions to this important area of research and engineering. The collection presents early findings and case studies on fundamental and applied aspects of Structural Dynamics, including papers on Aeroelasticity, Ground Testing, Dynamic Testing of Aerospace Structures, and Random Vibration.
590 _aPara consulta fuera de la UANL se requiere clave de acceso remoto.
710 2 _aSpringerLink (Servicio en línea)
_9299170
776 0 8 _iEdición impresa:
_z9781441993014
856 4 0 _uhttp://remoto.dgb.uanl.mx/login?url=http://dx.doi.org/10.1007/978-1-4419-9302-1
_zConectar a Springer E-Books (Para consulta externa se requiere previa autentificación en Biblioteca Digital UANL)
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