Sathyanarayana, CN and Krishna, Saraswathi and Dwarakanath, K and Nagaraja, BV and Vijaya Kumar, PS and Vijaya Vittala, NG and Viswanath, S and Shashikant, AK (2004) Ground Vibration Testing of SARAS Aircraft. Technical Report. National Aerospace Laboratories, Bangalore, India.
Full text available as:![[img]](http://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) | PDF Restricted to Archive staff only Download (17Mb) |
Abstract
Ground Vibration Test (GVT) on full aircraft is essential to determine the modal parameters,13; such as Natural Frequencies, Modal Damping and Mode Shapes. The results of GVT will also13; be used to update the numerical model. During the design stage of any aircraft development,13; free vibration charactenstics are estimated by analytical predictions using Finite Element13; Analysis of the aircraft. These characteristics are to be verified and updated through GVT.13; A detailed report on the test procedures that were followed for the GVT of SARAS VT-XSD13; using the 60-channel GVT system and results obtained is presented in this document. The13; experimentally determined modal parameters may be used as input for fine-tuning the13; aeroelastic analysis.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | SARAS aircraft;GVT;Modal test;certification |
| Subjects: | AERONAUTICS > Aircraft Design, Testing & Performance |
| Division/Department: | Structures Division, Structures Division, Structures Division, Structures Division, Structures Division, Structures Division, Structures Division, Structures Division |
| Depositing User: | Mrs Manoranjitha M D |
| Date Deposited: | 27 Jan 2006 |
| Last Modified: | 24 May 2010 09:39 |
| URI: | http://nal-ir.nal.res.in/id/eprint/939 |
Actions (login required)
| View Item |
