Nagarajan, V and Sundaramurthy, H (1982) Estimation of inertial peoperties of wind tunnel aircraft models Part I: Development of a computer programme13; Part II: Description of a rig and measurements on typical models. Technical Report. National Aeronautical Laboratory, 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 (15Mb) |
Abstract
The report contains a description of a computer programme13; and a test rig for the determination of the mass, location of13; center of gravity and moments of inertia of wind tunnel aircraft models. The computer programme is primarily meant for assisting the design of models used for dynamic tests accurate measurements of the inertial properties of the model required for data reduction and other purposes can be obtained using the test rig.13;
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Wind tunnel;Aircraft models |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics |
| Depositing User: | Mrs Manoranjitha M D |
| Date Deposited: | 21 Aug 2006 |
| Last Modified: | 24 May 2010 09:49 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2548 |
Actions (login required)
| View Item |
