Narayan, KY and Gopinath, N and Seshagiri, SN (1988) Wind tunnel tests on LCA 6.02 configuration. Project Report. National Aerospace Laboratories, Bangalore.
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Abstract
Tests were conducted in the NAL 1.2m trisonic wind tunnel on a 1/20th scale model of the LCA Stage 6.02 configuration. The tests were carried out in a Mach number range of 0.5 to 1.6 and over an angle of attack range which varied from -5 deg to +28 deg at M = 0.5 to -5 deg to +12 deg at M = 1.6. The test Reynolds number (based on wing mean aerodynamic chord) varied between 4.8 to 10.28 millions depending on the Mach number. The tests Included : (i) determination of the longitudinal characteristics of the configuration and (ii) determination of longitudinal, lateral and directional control powers.
| Item Type: | Proj.Doc/Technical Report (Project Report) |
|---|---|
| Uncontrolled Keywords: | LCA;High speed tests |
| Subjects: | AERONAUTICS > Aerodynamics |
| Division/Department: | Aerodynamics, Aerodynamics , Aerodynamics |
| Depositing User: | Smt Bhagya Rekha KA |
| Date Deposited: | 03 Sep 2012 13:40 |
| Last Modified: | 25 Sep 2012 10:00 |
| URI: | http://nal-ir.nal.res.in/id/eprint/10883 |
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- Wind tunnel on LCA stage V configuration. (deposited 03 Sep 2012 12:11)
- Wind tunnel tests on LCA 6.02 configuration. (deposited 03 Sep 2012 13:40)[Currently Displayed]
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