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Conference or Workshop Item

Bikshapathi, Manupati and Karthik, N and Buddhadeb, Nath and Gopinath, PR and Mohan, SR and Koner, D (2009) Study of flow unsteadiness in a bifurcated Y-Shaped duct for a typical combat aircraft model. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2009), December 10-12, Bangalore,India.

Mudkavi, Vidyadhar Y and Suryanarayana, GK and Thangavelu, RP (2009) Aerodynamic data sharing and database: A proposal. In: National Conference on Wind Tunnel Testing 2009-CP16, 12-14 Mar 2009, IISc., Bangalore.

Rajeev, G and Jinde, P (2009) Design and development of a 2.5quot; diameter integral 6-component strain gage balance. In: National Conference on Wind Tunnel Testing 2009-CP15, 12-14 Mar 2009, IISc., Bangalore.

Sampath, Rao (2009) Wind Tunnel Testing of Aerospace Structures. In: International Symposium on Opportunities and Challenges Facing Aviation Industry in Indian Subcontinent, 18-20, 2009, Sreenithi Institute of Science & Technology.

Sundaramurthy, H (2009) Statistical analysis of repeat test results for assessment of wind tunnel data quality. In: National Conference on Wind Tunnel Testing (2009-IT2), 12-14 Mar 2009, IISc., Bangalore.

Suryanarayana, GK (2009) Overview of NTAF activities and perspective for future. In: National Conference on Wind Tunnel Testing (2009-IT8), 12-14 Mar 2009, IISc., Bangalore.

Suryanarayana, GK and Basavaraju, NR and Suprabha, PS (2009) Concept of variable mach number flexible nozzle and controls for NAL 0.6m blowdown wind tunnel. In: National Conference on Wind Tunnel Testing 2009-CP18, 12-14 Mar 2009, IISc., Bangalore.

Proj.Doc/Technical Report

Nitin, Khamesra and Karthik, N (2009) Conformatory tests on 1:50 scale PSLV_XL configuration. Technical Report. National Aerospace Laboratories, Bangalore, India.

Nitin, Khamesra and Srinivasan, N (2009) Wind tunnel tests on 1:50 scale GSLV Mk II configuration. Technical Report. National Aerospace Laboratories, Bangalore, India.

Sharma, RC and Gopinath, N and Karthik, N (2009) Concept study of fin mounted tail plane for pitch-up alleviation of LCA. Technical Report. National Aerospace Laboratories, Bangalore, India.