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Items where Author is "Hartmann, K"
Group by: Item Type | No Grouping Jump to: Proj.Doc/Technical Report Number of items: 3.
Proj.Doc/Technical ReportKanagarajan, 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. |
