Rajamurthy, MS and Basappa, - and Bhagawan, - and Shubha, G (1993) Dynamic Wind Tunnel Testing Of A Flexible Delta Wing. Technical Report. NAL, Bangalore.
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Abstract
Dynamic Wind Tunnel Testing Of A Flexible Delta Wing Model W3.Carried Out To Generate Experimental Data 3To Be Used By ; The Aero-Servo-Elastic Analysis Group Of ADA . This Report Details Model Eoastruztion, Instrumentation, And Wind Tunnel Testing As Well As The Analysis Carried Out To Obtain Transfer Function As From Wind Tunnel Test Data.
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Aeroservoelasticity; Flexible Delta Wing; Dynamic Wind Tunnel Testing; Time Domain Identification; Sine Sweep Tests; Acceleration Transfer Function |
| Subjects: | AERONAUTICS > Aeronautics (General) |
| Division/Department: | Systems Engineering Division, Flight Mechanics and Control Division, Systems Engineering Division, Flight Mechanics and Control Division |
| Depositing User: | M/S ICAST NAL |
| Date Deposited: | 21 Sep 2012 10:58 |
| Last Modified: | 21 Sep 2012 10:58 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10980 |
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