Srivastava, A and Sharma, N and Srinivasa, C (1991) Aerodynamic analysis of NAL Light Aircraft Wing using a vortex lattice program. Technical Report. National Aeronautical Laboratory, Bangalore, India.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
pd_cf_9112_R85495.pdf Restricted to Repository staff only Download (7MB) |
![[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 (5kB) |
Abstract
A litting analysis of NAL-LA wing has been made using a vortex lattice program and the aexA3;quot;odynamic characteristics are computed by modelling the wing as a system of horse shoe vortices. The spanwise loading shows close agreement with elliptic loading and the section lift coefficient is nearly constant across the span except at the wing tip. The aerodynamic characteristics exhibit satisfactory convergence with increasing panel density.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Vortex;Lattice |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics AERONAUTICS > Aerodynamics |
| Depositing User: | Mr. N A |
| Date Deposited: | 28 Jun 2006 |
| Last Modified: | 24 May 2010 04:14 |
| URI: | http://nal-ir.nal.res.in/id/eprint/1842 |
Actions (login required)
 |
View Item |
