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Number of items: 15.

Balakrishna, 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.

Chetty, 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.

Jayaraman, V (1987) Surface Pressure Distributions on an Axisymmetric Underwater Body - Theory and Experiment. Project Report. National Aerospace Laboratories, Bangalore.

Jayaraman, V (1987) Wind .-Turinel Testing . on underwater Axisymmetric body at Angle of Attack,-Part II Experimental investigation on an Axisymmetric body with ogive nose. Project Report. National Aerospace Laboratories, Bangalore.

Jayaraman, V (1987) Wind Tunnel Testing of Screen elements used for a Radio Telescopic Antenna (GIMRT). Project Report. National Aerospace Laboratories, Bangalore.

Jayaraman, V (1987) Wind Tunnel Testing on Underwater Axisymmetric Bodies at Angle of Attack - Part IV - Surface Pressure Measurements on the Model at Negative Incidences. Project Report. National Aerospace Laboratories, Bangalore.

Jayaraman, V (1987) Wind Tunnel Testing on an Axisymmetric Body at Angles of Attack Part V - Boundary Layer Profile Measurement on an Axisymmetric Body. Project Report. National Aerospace Laboratories, Bangalore.

Karunakar, K and Murthy, NN and Niranjana, T and Rajan, SR and Shyam, Chetty and Padma, Madhuranath and Shylaja, G Prasad (1987) Design and simulation of a Digital Combat Flap controller for a fighter Aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Kumar, 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.

Mathur, NB and Krishnan, V and Yajnik, KS (1987) Base Flow Facility Progress Report for 1986-37. Project Report. National Aerospace Laboratories, Bangalore.

Mohan Ram, VS and Raol, JR and Jagadeesh, M (1987) Flight Test Specification for Missile Parameter Identification. Project Report. National Aerospace Laboratories, Bangalore.

Parameswaran, 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.

Rajappa, N and Leelavathi, K (1987) Pressure distributions on an under-water store : I. Project Report. National Aerospace Laboratories, Bangalore.

This list was generated on Wed May 25 01:10:35 2016 IST.