Items where Author is "Hartmann, K"

Up a level
Export as [feed] RSS 2.0 [feed] RSS 1.0 [feed] Atom
Group by: Item Type | No Grouping
Number of items: 3.

Proj.Doc/Technical Report

Kanagarajan, V and Hartmann, K (1989) Force Measurements At Low Spefeds On . Body Wing Tail Combinations (Kaha Model) At High Reynolds Numbers And Incidences From -2° To 70°. Technical Report. NAL, Bangalore.

Narayan, KY and Hartmann, K (1988) Transonic and supersonic flow past a 65xB0; delta wing with rounded leading edges - analysis of experimental data. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kanagarajan, V and Hartmann, K (1988) Force Measurements on a Body wing tail configuration (KaHa Model) at Mach numbers of 0.4 , 0.6 and 0.8 and incidences from 30° to 65°. Project Report. National Aerospace Laboratories, Bangalore.

This list was generated on Sat Nov 1 02:42:42 2014 IST.