Please use this identifier to cite or link to this item:
http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/2859
Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | NANDA, DILIP KUMAR | |
dc.date.accessioned | 2014-09-25T06:35:00Z | |
dc.date.available | 2014-09-25T06:35:00Z | |
dc.date.issued | 1981-08 | |
dc.identifier.govdoc | NB10950 | |
dc.identifier.uri | http://www.idr.iitkgp.ac.in/xmlui/handle/123456789/2859 | |
dc.language.iso | en | en |
dc.publisher | IIT Kharagpur | en |
dc.subject | Hess and Smith Technique | en |
dc.subject | Calculation of Compressible | en |
dc.subject | Layer Simulation | en |
dc.subject | Two- Dimensional Bodies | en |
dc.subject | Laminar Boundary Layer | en |
dc.subject | Mathematical Formulation | en |
dc.subject | Numerical Solution | en |
dc.subject | Blowing Simulation | en |
dc.subject | Displacement Simulation | en |
dc.subject | Viscosity | en |
dc.subject | Compressibility | en |
dc.title | Aerofoil and Wing Problems in Steady and Unsteady Motions | en |
dc.type | Thesis | en |
Appears in Collections: | Aerofoil and Wing Problems in Steady and Unsteady Motions |
Files in This Item:
File | Description | Size | Format | |
---|---|---|---|---|
NB10950_Abstract.pdf | 498.2 kB | Adobe PDF | ![]() View/Open | |
NB10950_Thesis.pdf Restricted Access | 9.02 MB | Adobe PDF | View/Open Request a copy |
Items in DSpace are protected by copyright, with all rights reserved, unless otherwise indicated.