पत्रिका (46)

• 2017 (3)
  • October (1)
    • Effect of transonic fresstream on linear cluster plug nozzle flow
  • July (1)
    • Effect of clustering on linear plug nozzle flow field for overexpanded internal jet
  • May (1)
    • Assessment of various low-profile mechanical vortex generators in controlling a shock-induced separation”
• 2016 (2)
  • October (1)
    • Experimental and numerical study of secondary flow and coolant film interaction in a high subsonic cascade tunnel
  • September (1)
    • Experimental investigation of an incident shock-induced interaction near an expansion corner
• 2015 (8)
  • December (1)
    • Experimental study of unsteady wake effect on a film-cooled pitchwise-curved surface
  • October (3)
    • Control of base pressure for a boat-tailed axisymmetric afterbody via base geometry modifications
    • Transition control of mach to regular reflection induced interaction using an array of micro ramp vane-type vortex generators
    • Control of shock-wave boundary layer interaction using steady micro-jets
  • September (2)
    • Experimental study of subsonic and sonic jets controlled by air tabs
    • Editorial on the thematic issue: supersonic flow control, shock waves
  • August (2)
    • Unsteady flow conditions during dual-bell sneak transition
    • Numerical simulation of shock/boundary layer interaction in supersonic overexpanded nozzles
• 2014 (2)
  • December (1)
    • Unsteady shock motions in an over-expanded parabolic rocket nozzle
  • May (1)
    • Effect of ambient pressure fluctuations on dual-bell transition behavior
• 2013 (4)
  • December (1)
    • Studies on the influence of steady microactuators on shock-wave/boundary-layer interaction
  • October (1)
    • Effect of truncation on the aeroacoustics of an annular aerospike nozzle’
  • May (2)
    • Reynolds number influence on dual-bell transition phenomena
    • Experimental studies on rectangular jets with trapezoidal tabs
• 2012 (3)
  • December (2)
    • Gas density effects on dual-bell transition behavior
    • Shockwave/boundary-layer interaction control on a compression ramp using steady microjets
  • July (1)
    • Control of shock unsteadiness in shock boundary-layer interaction on a compression corner using mechanical vortex generators
• 2011 (5)
  • December (4)
    • Cold gas testing of a thrust optimized parabolic nozzle in a high altitude simulation chamber
    • Cold gas dual-bell transition tests in a high altitude simulation chambe
    • Freestream effects on base pressure development of an annular plug nozzle’’
    • An experimental study of the linear plug flow-field and base pressure development in freestream flow
  • March (1)
    • Study of jets from rectangular nozzles with square grooves’
• 2010 (4)
  • December (2)
    • Flow separation characteristics of overexpanded nozzles
    • Studies on an elliptic jet with cylindrical tabs’
  • October (1)
    • Experimental study on a jet issuing from an elliptic nozzle with cylindrical tabs
  • June (1)
    • Stflow separation characteristics of a dual-bell nozzle during its transition modes
• 2009 (4)
  • October (1)
    • Study on restricted shock separation phenomena in a thrust optimized parabolic (top) nozzle
  • May (3)
    • Performance characteristics of an annular conical aerospike nozzle with freestream effect
    • Surface flow studies of restricted shock separation in a thrust optimized parabolic nozzle
    • Shock unsteadiness in a thrust optimized parabolic rocket nozzle
• 2006 (1)
  • September (1)
    • Relation between shock unsteadiness and the origin of side-loads in a thrust optimized parabolic rocket nozzle
• 2003 (3)
  • April (3)
    • Influence of aspect-ratio on the mixing and acoustic characteristics of plain and notched elliptic-slot jets
    • Experimental study of flow unsteadiness in a mach 9 compression ramp interaction using a laser schlieren system
    • On the origin of side-loads in rocket nozzles
• 2002 (3)
  • June (1)
    • Unsteady separation in a flare induced hypersonic shock-wave boundary-layer interaction flowfield
  • April (2)
    • Detection of fluctuating density gradient flowfield in shock-wave boundary-layer interactions using laser schlieren system
    • Study of flow separation in a truncated ideal contour (tic) nozzle
• 2001 (1)
  • January (1)
    • Flow and acoustic properties of underexpanded elliptic-slot jets
• 1999 (2)
  • October (2)
    • Experimental study on the noise characteristics of notched circular-slot jets
    • Flow and noise characteristics of notched elliptic-orifice jets
• 1996 (1)
  • April (1)
    • Supersonic separation with obstructions