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Rao, R Anand and Nath, B and Gopinath, N and Reddy, Krishna Rakend D (2011) Reynolds Number and Leading Edge Bluntness Effects on 65° Delta Wing at Subsonic Speed. In: Symposium on Applied Aerodynamics and Design of Aerospace Vehicle (SAROD 2011), November 16-18, 2011, 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.
Gopinath, N and Seshadri, SN and Dutt, HNV and Sampath, Rao B (1991) Wind Tunnel Tests On 1/20 Scale 6.45v35 Configuration Part I: Longitudinal Characteristics. Technical Report. NAL, Bangalore.
Gopinath, N and Narayan, KY (1988) Wind tunnel tests on LCA stage 4 configuration. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, KY and Gopinath, N and Seshagiri, SN (1988) Wind tunnel tests on LCA 6.12 configuration. Project Report. National Aerospace Laboratories, Bangalore.
Narayana Rao, CK and Gopinath, N (1987) Effect of protuberances on the aerodynamic characteristics of ASLV. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, KY and Gopinath, N (1986) Wind tunnel tests on lca delta-5 configuration part II: results at supersonic speeds and analysis. Project Report. National Aerospace Laboratories, Bangalore.
Narayan, KY and Gopinath, N and Seshadri, SN (1985) Wind tunnel tests on MiG-2114 aircraft model with combat flaps. Project Report. NAL, Bangalore.
