Srilatha, KR and Ramamoorthy, P (1990) Design of a Natural laminar Flow Airfoil for a Regional Transport Aircraft. 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 (3034Kb) |
Abstract
A 16% thick NLF airfoil is designed for a future regional13; aircraft which is expected to incorporate advance technology13; concepts in Aerodynamics, structures and Controls. This airfoil13; is compared with DO-NTLF-160 airfoil of same thickness. . .13; NAL airfoil, designated as. NAL-MSNLF-160, has given the same13; Performance as NTLF airfoil if not better.13; 13;
| Item Type: | Proj.Doc/Technical Report (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Airfoil;Design;Pressure Distribution;General13; Aviation;Regional Transport.13; 13; |
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Division/Department: | Computational and Theoretical Fluid Dynamics Division, Computational and Theoretical Fluid Dynamics Division |
| Depositing User: | Mrs Manoranjitha M D |
| Date Deposited: | 15 Jul 2006 |
| Last Modified: | 24 May 2010 09:45 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2074 |
Actions (login required)
| View Item |
