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.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
tr_pdcf_9002_R86309_txt.pdf Restricted to Repository staff only Download (3MB) |
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/other.png) |
Indexer Terms (Generate index codes conversion from application/pdf to indexcodes)
indexcodes.txt Restricted to Repository staff only Download (2kB) |
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: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Airfoil;Design;Pressure Distribution;General13; Aviation;Regional Transport.13; 13; |
| Subjects: | AERONAUTICS > Aircraft Propulsion and Power |
| Depositing User: | Mrs Manoranjitha M D |
| Date Deposited: | 15 Jul 2006 |
| Last Modified: | 24 May 2010 04:15 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2074 |
Actions (login required)
 |
View Item |
