Items where Author is "Kanagarajan, V"

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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.

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.

Selvarajan, S and Arokkiaswamy, A and Kanagarajan, V (1988) Wind Tunnel Force Measurements on 1/12 Scale Model of PRITHVI missile Configuration - II : Final Report. Project Report. National Aerospace Laboratories, Bangalore.

Kanagarajan, V and Arokkiaswamy, A (1986) Some studies on induced rolling moment of a missile type configuration 13; 13;. In: 2nd National Conference on Aerodynamics, 19-20 Dec 1986, Bangalore, India.

Kanagarajan, V and Arokkiaswamy, A (1986) Experimental Studies on a 1/12 Scale Model of Prithvi Missile. Project Report. NAL, Bangalore.

Arokkiaswamy, A and Kanagarajan, V (1985) Estimation of error in measurement of force and moment coefficients of wind tunnel models. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Swamy, M Shivakumara and Narasimhan, TM and Narayan, KY and Murthy, HS and Rajendra, G and Kanagarajan, V (1985) Semi-Captive Trajectory Technique. Project Report. National Aerospace Laboratories, Bangalore.

Gopinath, R and Kanagarajan, V (1983) Adaptation of TSFOIL for univac 1100/60H computer at NAL, Bangalore. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kanagarajan, V (1977) Aerodynamics performance of the wing with leading edge strakes. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Kanagarajan, V (1976) Experimental studies on a wing with strake. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rao, DM and Rajendra, G and Sundaramurthy, H and Kanagarajan, V (1975) Contributions by NAL Aerodynamics Division at SLV-3 Review. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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