Items where Author is "Mathur, NB"

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Mathur, NB and Sajeer, Ahmed (2012) Test technique for the measurement of intake drag of air-breathing vehicles. Journal of Aircraft, 49 (6). pp. 2093-2095. ISSN 0021-8669

Ahmed, Sajeer and Mathur, NB and Manisankar, C (2011) Evaluation of aerodynamic performance of sidewall compression intake relevant to air breathing propulsion vehicles for intake flow entry at M = 3.5. Project Report. National Aerospace Laboratories, Bangalore.

Mathur, NB and Viji, M (2010) Experimental studies on twinjet afterbody-nozzle system of combat aircraft configurations. Project Report. National Aerospace Laboratories, Bangalore.

Mathur, NB and Viji, M (2009) Experimental Studies on Twin Jet Afterbody-Nozzles System of Combat Aircraft Configuration. Project Report. National Aerospace Laboratories, Bangalore.

Sajeer, Ahmed and Mathur, NB and Manisankar, C (2008) Evaluation of Aerodynamic Performance of Sidewall Compression Intake Relevant to Airbreathing Propulsion Vehicles for Intake Flow Entry at M=4.0. Technical Report. National Aerospace Laboratories, Bangalore, India.

Verma, SB and Mathur, NB (2008) Experimental study of conical aerospike nozzles. Project Report. National Aerospace Laboratories, Bangalore.

Mathur, NB and Viji, M (2008) Measurements of aerodynamic loads on afterbody-nozzle configuration of HSTDV-SERN nozzle system. Project Report. National Aerospace Laboratories, Bangalore.

Venkatakrishnan, L and Suriyanarayanan, P and Mathur, NB (2007) BOS density measurements in afterbody flows with shock13; and jet effects AIAA 2007-4223. In: 37th AIAA Fluid Dynamics Conference and Exhibit, 25-28 Jun 2007, Miami, FL..

Venkatakrishnan, L and Suriyanarayanan, P and Mathur, NB (2007) BOS Density Measurements in Afterbody Flows with Shock and Jet Effects. In: 37th AIAA Fluid Dynamics Conference and Exhibit 25-28 , June 2007, Miami, FL.

Verma, SB and Mathur, NB (2007) Experimental Studies of Conical Aerospike Nozzles. Project Report. National Aerospace Laboratories, Bangalore.

Venkatakrishnan, L and Mathur, NB (2006) PIV Studies in Under Expanded Supersonic Jets. Project Report. National Aerospace Laboratories, Bangalore.

Verma, SB and Mathur, NB (2006) Experimental study of conical aerospike nozzles. Project Report. National Aerospace Laboratories, Bangalore.

Mathur, NB and Rajeev, Kumar (2004) Experimental Studies on 1/15th Scale SARAS Afterbody Model with Underside Fuselage Fairing, Ventral Fins, Nacelles and Stub Main Wing. Technical Report. National Aerospace Laboratories, Bangalore, India.

Mathur, NB and Viswanath, PR (2004) Drag Reduction from Square-Base Afterbodies at High Speeds. Journal of Aircraft, 41 (4). pp. 811-820.

Mathur, NB (1999) Estimation of afterbody drag with jet temperature effects for the afterbody-nozzle configuration of a combat aircraft. Journal of Aeronautical Society of India, 51 (3). pp. 181-185.

Mathur, NB (1998) Correlation for the Estimation of Afterbody Drag with Hot Jet Exhaust. Journal of Aircraft, 35 (6). pp. 981-984.

Krishnan, V and Mathur, NB (1997) Afterbody Boundary Layer Measurements in the Base Flow Facility. Technical Report. National Aerospace Laboratories, Bangalore,India.

Mathur, NB (1995) Afterbody-Nozzle Drag Characteristics Of LCA-KAVERI CONFIGURATION. Technical Report. NAL, Bangalore.

Mathur, NB (1991) Development of underexpanded sonic jet exhausting from the convergent nozzle of an axisymmetric afterbody configuration. In: International Symposium on Air Breathing Engines, 1-6 Sep 1991, Nottingham, England.

Mathur, NB (1990) After body Pressure Drag Data For The Reheat, Intermediate And Dry Nozzle Operating Conditions Of The LCA-GTX 35vs Configuration. Technical Report. NAL, Bangalore.

Mathur, NB and Yajnik, KS (1990) Underexpanded jet-freestream interactions on an axisymmetric afterbody configuration. AIAA Journal, 28 (1). pp. 47-50. ISSN 0001-1452

Anantha, KV and Mathur, NB and Krishnan, V (1989) Design characteristics of the variable supersonic nozzle of the base flow facility. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mathur, NB and Yajnik, KS (1989) Axisymmetric afterbody flow separation at transonic speeds in presence of jet exhaust. In: 9th International Symposium on Air Breathing Engines, 03-08 Sept 1989, Athens, Greece.

Mathur, NB and Sreekanth, AK (1988) Separated transonic interaction characterstics of an afterbody configuration in presence of a central propulsive jet. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Mathur, NB and Ramesh, G and Yajnik, KS (1988) Continuous coloured smoke-wire technique for flow visualisation. Journal of Aeronautical Society of India, 40 . pp. 131-137.

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

Mathur, NB and Yajnik, KS (1987) Underexpanded jet-free stream interactions on an axisymmetric afterbody configuration. In: 8th International Symposium on Air Breathing Engines, 14-19 June 1987, Ohio, United States.

Krishnan, V and Mathur, NB and Yajnik, KS (1986) Base Flow Facility Progress Report For 1985-86. Technical Report. NAL, Bangalore.

Krishnan, V and Mathur, NB and Yajnik, KS (1986) Base Flow Facility Progress Report For 1985-86. Technical Report. NAL, Bangalore.

Mathur, NB and Ramesh, G and Karunakaran, KM and Yajnik, KS (1986) Continous colouhed smoke-wire technique for flow visulisation in wind tunnels. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Mathur, NB and Yajnik, KS (1985) Jet plume temperature effects on afterbody pressure distribution and drag. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Mathur, NB and Yajnik, KS (1985) Jet plume temperature effects on afterbody pressure distribution and drag. In: 7th International Symposium on Air Breathing Engines, 2-6 Sep 1985, Beijing, China.

Mathur, NB and Ramakrishnan, MS (1984) A rig for testing afterbodies of aerospace vehicles in presence of j e t in 0.3m trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore,India.

Mathur, NB (1984) Effects of under expanded jet on afterbody drag of an axisymmetric configuration. Technical Report. National Aeronautical Laboratory, Bangalore, India.

Lokhandwala, OA and Mathur, NB and Mohan, J (1980) Jet simulation studies in the 1.2m wind tunnel (of effects of stage separation). Aeronautical Society of India, Journal, 32 . pp. 137-142.

Mathur, NB and Mohan, Jai and Lokhandawala, OA (1978) Cold jet simulation RIG for the NAL 1.2M trisonic wind tunnel. Technical Report. National Aeronautical Laboratory, Bangalore, India.

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