Items where Author is "Verma, SB"

Verma, SB and Manisankar, C (2012) Shockwave/boundary-layer interaction control on a compression ramp using steady microjet. AIAA Journal, 50 (12). pp. 2753-2764. ISSN 0001-1452

Verma, SB and Stark, R and Haidn, O (2012) Gas Density Effects on Dual-Bell Transition Behavior. Journal of Propulsion and Power, 28 (6). pp. 1315-1323. ISSN 0748-4658

Verma, SB and Stark, R and Haidn, O (2011) Gas density effects on dual-bell transition behavior. In: 4th European Conference for AeroSpace Sciences (EUCASS), 4-8 Jul. 2011, St. Petersburg, Russia.

Verma, SB and Raju, Channa and Manisankar, C (2011) Shock-Wave Boundary-Layer Interaction Study on a 20' Compression Corner Using PSP and Kulites. Project Report. National Aerospace Laboratories, Bangalore.

Verma, SB and Stark, R and Genin, C and Haidn, O (2011) Cold gas dual-bell tests in high-altitude simulation chamber. Shock Waves, 21 . pp. 131-140.

Verma, SB and Viji, M (2011) Freestream effects on base pressure development of an annular plug nozzle. Shock Waves, 21 (2). pp. 163-171.

Kumar P, Arun and Verma, SB and Elangovan, S (2011) Study of jets from rectangular nozzles with square grooves. Aeronautical Journal, 115 (1165). pp. 187-196. ISSN 0001-9240

Verma, SB and Haidn, Oskar (2010) Flow characteristics of overexpanded rocket nozzles. International Journal of Aerospace Innovations, 2 (4). pp. 259-277. ISSN 1757-2258

Verma, SB and Channa Raju, - and Manisankar, C (2010) Shock-wave boundary-layer interaction study on a 20 deg compression corner using PSP and Kulites. Project Report. National Aerospace Laboratories, Bangalore.

Verma, SB and Stark, R and Nuerenberger-Genin, C and Hakin, O (2010) Cold-gas experiments to study the flow separation characteristics of a dual-bell nozzle during its transition modes. Shock Waves, 20 . pp. 191-203.

Verma, SB and Sudhakar, and Venkatakrishnan, L (2009) Experimental study on a jet issuing from an elliptic nozzle with cylindrical tabs. Journal of Turbulence, 11 (20). pp. 1-24.

Verma, SB and Manisankar, C (2009) HSTDV Nozzle Contour Optimization for Enhanced Force Characteristics – Phase I. Project Report. National Aerospace Laboratories, Bangalore.

Verma, SB and Viji, M (2009) Experimental Evaluation of Linear Plug Nozzle Flow-field. Project Report. National Aerospace Laboratories, Bangalore.

Venkatakrishnan, L and Karthikeyan, N and Verma, SB (2009) Effect of spike truncation on of the acoustics of an annular aerospike Nozzle Flow. In: 30th AIAA Aerocoustics Conference, 11-13 May 2009, Miami, Florida, USA.

Ramesh, G and Verma, SB (2009) Investigation of near Field Flow of an Elliptic Jet in a Co-flowing Outer Stream using 2D PIV. Project Report. National Aerospace Laboratories, Bangalore.

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

Verma, SB and Venkatakrishnan, L and Ramesh, G (2007) 2-D PIV study of near-field flow development from a 2:1 elliptic jet with tabs AIAA-2007-4498. In: 37th AIAA Fluid Dynamics Conference and Exhibit, 25-28 Jun 2007, Miami, FL..

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

Verma, SB and Haidn, Oskar (2007) Flow Separation Studies in a Subscale Truncated Ideal Contour Nozzle. In: 45th AIAA Aerospace Sciences Meeting and Exhibit, 8-11 Jan 2007, USA.

Venkatakrishnan, L and Verma, SB (2006) Aeroacoustics instrumentation and noise measurements Part II: Propeller noise measurements. Project Report. National Aerospace Laboratories, Bangalore.

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