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Number of items: 2.

Proj.Doc/Technical Report

Gopinath, R and Murthy, AV (1969) Study of the effect of pressure gradient on compressible laminar large boundary layers at large prandtl numbers. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Ramamoorthy, P and Narayana, CL (1969) Spline approximation as applied to aeronautical problems. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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