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Nonlinear Vibration With Control by David Wagg
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1DTIC ADA113239: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control Problems.
By Defense Technical Information Center
This report summarizes the accomplishments of a study exploring new methods for the vibration control of helicopters. Reanalysis methodology permits a variety of vibration control problems to be solved efficiently. Both analytical and experimental studies have been conducted. (Author)
“DTIC ADA113239: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control Problems.” Metadata:
- Title: ➤ DTIC ADA113239: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control Problems.
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA113239: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control Problems.” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Pilkey,Walter D - VIRGINIA UNIV CHARLOTTESVILLE DEPT OF MECHANICAL AND AEROSPACE ENGINEERING - *VIBRATION - *HELICOPTERS - CONTROL - ABSORBERS(EQUIPMENT) - DYNAMIC RESPONSE - RESONANT FREQUENCY - HELICOPTER ROTORS - MATHEMATICAL MODELS - EXCITATION - STRUCTURAL RESPONSE - AIRCRAFT EQUIPMENT - FREQUENCY RESPONSE - NUMERICAL ANALYSIS
Edition Identifiers:
- Internet Archive ID: DTIC_ADA113239
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 17.46 Mbs, the file-s for this book were downloaded 49 times, the file-s went public at Thu Jan 04 2018.
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2DTIC ADA161457: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control.
By Defense Technical Information Center
Several problems concerning the vibration control of helicopters were studied. A method for introducing structural modifications leading to vibration reduction has been developed. In particular, a formulation for attaching appendages to continuous structural members was completed and applied to a two-beam helicopter model. (Author)
“DTIC ADA161457: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control.” Metadata:
- Title: ➤ DTIC ADA161457: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control.
- Author: ➤ Defense Technical Information Center
- Language: English
“DTIC ADA161457: Limiting Performance Of Nonlinear Systems With Applications To Helicopter Vibration Control.” Subjects and Themes:
- Subjects: ➤ DTIC Archive - Pilkey,W D - VIRGINIA UNIV CHARLOTTESVILLE DEPT OF MECHANICAL AND AEROSPACE ENGINEERING - *VIBRATION - MATHEMATICAL MODELS - CONTROL - BEAMS(STRUCTURAL) - DISPLACEMENT - EIGENVALUES - RESONANT FREQUENCY - NONLINEAR SYSTEMS - HELICOPTERS - LIMITATIONS - RESONANCE - TUNING - ATTACHMENT - FREQUENCY RESPONSE - APPENDAGES
Edition Identifiers:
- Internet Archive ID: DTIC_ADA161457
Downloads Information:
The book is available for download in "texts" format, the size of the file-s is: 5.28 Mbs, the file-s for this book were downloaded 58 times, the file-s went public at Sun Feb 04 2018.
Available formats:
Abbyy GZ - Archive BitTorrent - DjVuTXT - Djvu XML - Item Tile - Metadata - OCR Page Index - OCR Search Text - Page Numbers JSON - Scandata - Single Page Processed JP2 ZIP - Text PDF - chOCR - hOCR -
Related Links:
- Whefi.com: Download
- Whefi.com: Review - Coverage
- Internet Archive: Details
- Internet Archive Link: Downloads
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