Ramamoorthy, P and Dhanalakshmi, K (1987) NCSU Code: Validation and extension on NAL's UNIVAC 1100/60 system. Technical Report. National Aeronautical Laboratory, Bangalore, India.
![[img]](https://nal-ir.nal.res.in/style/images/fileicons/application_pdf.png) |
PDF
tr_pdfm_8716_R69714_txt.pdf Restricted to Repository staff only Download (15MB) |
![[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 (8kB) |
Abstract
An existing computer program for obtaining the pressures on an airfoil named here as (NCSU CODE), which was developed by Prof. Smetana and his coworkers at North Carolina State University, is validated on UNIVAC 1100/60 att NAL. A graphlc routine to plot the results is added to this program to emhance its utility.13; 13; The code is tried on a large number of airfoils inc1uding the modern general aviation and natural laminar airfoils. The results agree quite well with the experimental results; one should however realise that such a comparison is between the calculation In a free jet with experiments in tunnels of different blockage ratios and free stream turbulence.
| Item Type: | Monograph (Technical Report) |
|---|---|
| Uncontrolled Keywords: | Airfoil;Pressure distribution13; |
| Subjects: | ENGINEERING > Fluid Mechanics and Thermodynamics |
| Depositing User: | Poornima Narayana |
| Date Deposited: | 11 Aug 2006 |
| Last Modified: | 24 May 2010 04:15 |
| URI: | http://nal-ir.nal.res.in/id/eprint/2061 |
Actions (login required)
 |
View Item |
