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Number of items: 7.
BBalakrishna, S and Niranjana, T (1987) A Low Speed Tunnel Semi Free Dynamic Flying Study of Pitching Derivatives of LCA Delta-5 in Active Control using MLE Procedure. Project Report. National Aerospace Laboratories, Bangalore. Balakrishna, S and Niranjana, T (1987) Wind tunnel dynamic flying study of the pitching moment derivatives of the Standard Dynamics Model in active control. In: AIAA Atmospheric Flight Mechanics Conference, 17-19 Aug 1987, United States. CChetty, Shyam and Henschel, F and Hanke, D (1987) ATTAS in-flight simulation and model-following control (Advanced Technologies Testing Aircraft System)). In: National Seminar on Flight Research, Test and Development, May-Aug 1987, Bangalore, India. KKumar, Anand (1987) Euler solutions with a multi-block structured code. Technical Report. National Aeronautical Laboratory, Bangalore,India. Kumar, Anand and Das, A (1987) Numerical solution of flow fields around delta wings using euler equations method. Technical Report. National Aeronautical Laboratory, Bangalore,India. MMohan Ram, VS and Raol, JR and Jagadeesh, M (1987) Flight Test Specification for Missile Parameter Identification. Project Report. National Aerospace Laboratories, Bangalore. PParameswaran, V and Girija, G (1987) Flight Test Specifications and Preliminary data Analysis for Parameter Identification of HS 748 Aircraft. Project Report. National Aerospace Laboratories, Bangalore. |