Items where Author is "Seshadri, SN"

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Yegna Narayan, K and Seshadri, SN (1997) Types of flow on the lee side of delta wings13. Progress in Aerospace Sciences, 33 (3-4). pp. 167-257.

Yegna Narayan, K and Seshadri, SN (1997) Types of flow on the lee side of delta wings. Progress in Aerospace Sciences, 33 (3-4). pp. 167-257. ISSN 0376-0421

Yegna Narayan, K and Seshadri, SN (1995) Types of Flow on the Lee Si-de of Delta Wings. Technical Report. National Aerospace Laboratories, Bangalore, India.

Seshadri, SN (1993) Prediction Of Drag Of Missiles At Subsonic, Transonic And Supersonic Speeds. Technical Report. NAL, Bangalore.

Seshadri, SN and Dutta, HNV (1992) Wing And Fin Load Characteristics Of 1/15 Scale Lca Sge 26d Flow Through Model Tested At 8' X 8' Transonic Pd Ea 9211 Wind-Tunnel, Calspan U .S .A . Technical Report. NAL, Bangalore.

Dutt, HNV and Seshadri, SN (1991) Data Base Management And Analysis System For Wind Tunnel Results (Version-Ii,). Technical Report. NAL, Bangalore.

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.

Narayan, KY and Seshadri, SN (1988) Vortical flows on the lee surface of delta wings. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Seshadri, SN and Narayan, KY (1988) Possible types of flow on lee-surface of delta wings at supersonic speeds. Aeronautical Journal, 92 . pp. 185-199. ISSN 0001-9240

Seshadri, SN and Narayan, KY (1987) Shock-induced separated flows on the lee surface of delta wings. Aeronautical Journal, 91 . pp. 128-141.

Seshadri, SN and Narayan, KY (1986) Lee Surface Flovv Over Delta Wings at Supersonic Speeds - Some Features of Different Types of Flow. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Narayan, G and Mahalingam, V and Rajagopalan, E and Seshadri, SN (1985) Data Acquisition Processing and Interactive Control Systems (DAPICS) : An Evaluation of various Offers. Project Report. National Aerospace Laboratories, Bangalore.

Bhagawan, BS and Parameswaran, V and Rajeswari, Ramamurthy and Sridhar, JK and Srinatha Sastry, CV and Ramabhadran, S and Seshadri, SN and Sundaramurthy, H and Yegnanarayan, K (1985) Stability and Control characteristics of MIG-21 aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Seshadri, SN (1985) Aerodynamic data base generation for combat aircraft configurations - A project proposal. Technical 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.

Narayan, KY and Seshadri, SN (1985) Parametric analysis of combat aircraft performance requirements. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Bhagawan, BS and Parameswaran, V and Rajeswari, Ramamurthy and Seshadri, SN and Sridhar, JK and Srinatha Sastry, CV and Yegnanarayan, K (1985) Longitudinal stability and control characteristics of MIG-21 aircraft. Project Report. National Aerospace Laboratories, Bangalore.

Rao, DM and Seshadri, SN (1976) Application of Radial-Splitters for Improved wide-angle diffuser performance in blowdown tunnel. Journal of Aircraft, 13 (7). pp. 538-540. ISSN 0021-8669

Seshadri, SN and Rajendra, G (1974) Appplication of the method of axial source for calculation of subcritical pressure distribution on 'Not'slender axisymmetric bodies at zero lift. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Seshadri, SN and Rao, DM (1974) On the application of radial-splitters flow spreaders in the NAL 1-FT. blowdown tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Rajendra, G and Seshadri, SN and Jerath, VK (1971) Programs for evaluating body radius in accordance with transonic area rule. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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