PUBLICATION OF प्रायोगिक वायुगतिकी प्रभाग

HEAT TRANSFER IN ROTATING RAYLEIGH ̶ BÉNARD CONVECTION WITH ROUGH PLATES, EFFECT OF MEAN AND FLUCTUATING PRESSURE GRADIENTS ON BOUNDARY LAYER TURBULENCE, DENSITY MEASUREMENTS USING BACKGROUND ORIENTED SCHLIEREN TECHNIQUE, INFLUENCE OF PROPELLER SLIPSTREAM ON VORTEX FLOW FIELD OVER A TYPICAL MICRO AIR VEHICLE, ACOUSTIC CHARACTERIZATION OF JET INTERACTION WITH LAUNCH STRUCTURES DURING LIFT-OFF, INFLUENCE OF LEADING EDGE TUBERCLES ON AERODYNAMIC CHARACTERISTICS OF A HIGH ASPECT-RATIO UAV, NEAR WAKE FIELD OF CIRCULAR CYLINDER WITH A FORWARD SPLITTER PLATE, EFFECT OF TRANSONIC FRESSTREAM ON LINEAR CLUSTER PLUG NOZZLE FLOW, EXPERIMENTAL INVESTIGATION ON THE NEAR FLOW FIELD OF DUAL STREAM NOZZLES, PIV INVESTIGATION ON THE LIFT ENHANCING CAPABILITIES OF SELF-ADAPTIVE FLAPS ON LOW ASPECT RATIO WINGS, EFFECT OF CLUSTERING ON LINEAR PLUG NOZZLE FLOW FIELD FOR OVEREXPANDED INTERNAL JET, ASSESSMENT OF VARIOUS LOW-PROFILE MECHANICAL VORTEX GENERATORS IN CONTROLLING A SHOCK-INDUCED SEPARATION”, EXPERIMENTAL AND NUMERICAL STUDY OF SECONDARY FLOW AND COOLANT FILM INTERACTION IN A HIGH SUBSONIC CASCADE TUNNEL, EFFECT OF PARTICLE INJECTION ON HEAT TRANSFER IN ROTATING RAYLEIGH ̶ BÉNARD CONVECTION, TRANSITIONS IN TURBULENT ROTATING CONVECTION: A LAGRANGIAN PERSPECTIVE, FLOW ANISOTROPY IN ROTATING BUOYANCY-DRIVEN TURBULENCE, NON-INTRUSIVE FLOW DIAGNOSTICS FOR AEROSPACE APPLICATIONS, EXPERIMENTAL INVESTIGATION OF AN INCIDENT SHOCK-INDUCED INTERACTION NEAR AN EXPANSION CORNER, FLOW INVESTIGATION OF LINEAR CLUSTER PLUG NOZZLE, EXPERIMENTAL STUDY OF UNSTEADY WAKE EFFECT ON A FILM-COOLED PITCHWISE-CURVED SURFACE, 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, EXPERIMENTAL STUDY OF SUBSONIC AND SONIC JETS CONTROLLED BY AIR TABS, EDITORIAL ON THE THEMATIC ISSUE: SUPERSONIC FLOW CONTROL, SHOCK WAVES, UNSTEADY FLOW CONDITIONS DURING DUAL-BELL SNEAK TRANSITION, NUMERICAL SIMULATION OF SHOCK/BOUNDARY LAYER INTERACTION IN SUPERSONIC OVEREXPANDED NOZZLES, UNSTEADY SHOCK MOTIONS IN AN OVER-EXPANDED PARABOLIC ROCKET NOZZLE, SHOCK WAVE BOUNDARY LAYER INTERACTION IN SUPERSONIC FLOW OVER A FORWARD-FACING STEP, IDENTIFICATION OF EMERGENT MOTION COMPARTMENTS IN THE AMNIOTE EMBRYO", EFFECT OF AMBIENT PRESSURE FLUCTUATIONS ON DUAL-BELL TRANSITION BEHAVIOR, ANALYSIS OF ANNULAR PLUG NOZZLE FLOWFIED,” JOURNAL OF SPACECRAFT AND ROCKETS, STUDIES ON THE INFLUENCE OF STEADY MICROACTUATORS ON SHOCK-WAVE/BOUNDARY-LAYER INTERACTION, ROLE OF COHERENT STRUCTURES IN SUPERSONIC IMPINGING JETS, DENSITY FIELD VISUALIZATION OF A MICRO-EXPLOSION USING BACKGROUND ORIENTED SCHLIEREN, EFFECT OF TRUNCATION ON THE AEROACOUSTICS OF AN ANNULAR AEROSPIKE NOZZLE’, REYNOLDS NUMBER INFLUENCE ON DUAL-BELL TRANSITION PHENOMENA, EXPERIMENTAL STUDIES ON RECTANGULAR JETS WITH TRAPEZOIDAL TABS, GAS DENSITY EFFECTS ON DUAL-BELL TRANSITION BEHAVIOR, FLOWFIELD ANALYSIS OF LINEAR PLUG NOZZLE, SHOCKWAVE/BOUNDARY-LAYER INTERACTION CONTROL ON A COMPRESSION RAMP USING STEADY MICROJETS, EXPERIMENTAL STUDIES ON A RUDIMENTARY FOUR WHEEL LANDING GEA, CONTROL OF SHOCK UNSTEADINESS IN SHOCK BOUNDARY-LAYER INTERACTION ON A COMPRESSION CORNER USING MECHANICAL VORTEX GENERATORS, FREESTREAM EFFECTS ON BASE PRESSURE DEVELOPMENT OF AN ANNULAR PLUG NOZZLE’’, COLD GAS DUAL-BELL TRANSITION TESTS IN A HIGH ALTITUDE SIMULATION CHAMBE, AN EXPERIMENTAL STUDY OF THE LINEAR PLUG FLOW-FIELD AND BASE PRESSURE DEVELOPMENT IN FREESTREAM FLOW, COLD GAS TESTING OF A THRUST OPTIMIZED PARABOLIC NOZZLE IN A HIGH ALTITUDE SIMULATION CHAMBER, GENERATION AND CONTROL OF OBLIQUE SHOCKS USING MICROJETS, NEW APPROACHES FOR ANALYSIS OF JET NOISE DATA, STUDY OF JETS FROM RECTANGULAR NOZZLES WITH SQUARE GROOVES’, FLOW SEPARATION CHARACTERISTICS OF OVEREXPANDED NOZZLES, STUDIES ON AN ELLIPTIC JET WITH CYLINDRICAL TABS’, STUDY OF INTERMITTENT TRANSITIONAL BOUNDARY LAYER USING PIV, EXPERIMENTAL STUDY ON A JET ISSUING FROM AN ELLIPTIC NOZZLE WITH CYLINDRICAL TABS, DENSITY FIELD MEASUREMENTS OF A SUPERSONIC IMPINGING JET WITH MICROJET CONTROL, APPLICATION OF PHOTOGRAMMETRY TO SURFACE FLOW VISUALIZATION, STFLOW SEPARATION CHARACTERISTICS OF A DUAL-BELL NOZZLE DURING ITS TRANSITION MODES, STUDY ON RESTRICTED SHOCK SEPARATION PHENOMENA IN A THRUST OPTIMIZED PARABOLIC (TOP) NOZZLE, THREE-DIMENSIONAL TOMOGRAPHIC RECONSTRUCTION OF DENSITY FIELD IN AN AFTERBODY FLOW WITH SHOCK AND JET EFFECTS, 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, RESECTION METHODOLOGY FOR PSP DATA PROCESSING: RECENT EXPERIENCES IN NAL, COMPUTATIONAL STUDIES ON FLOW THROUGH DE LAVAL NOZZLE, INVESTIGATION OF HYSTERESIS EFFECTS ON A WING-FLAP CONFIGURATION AT HIGH-LIFT USING PIV, PIV STUDIES OF LARGE SCALE STRUCTURES IN THE NEAR FIELD OF SMALL ASPECT RATIO ELLIPTIC JETS, FORWARD FLIGHT EFFECTS ON FAN NOISE FROM SUPERSONIC 2-D INLETS, PRESSURE SENSITIVE PAINT MEASUREMENTS ON A DELTA WING IN SUPERSONIC FLOW, RELATION BETWEEN SHOCK UNSTEADINESS AND THE ORIGIN OF SIDE-LOADS IN A THRUST OPTIMIZED PARABOLIC ROCKET NOZZLE, DENSITY MEASUREMENTS IN AN AXISYMMETRIC UNDEREXPANDED JET USING BACKGROUND ORIENTED SCHLIEREN TECHNIQUE, A COMPARATIVE STUDY OF DIFFERENT PSP IMAGE REGISTRATION TECHNIQUES, TURBULENCE AND NOISE SUPPRESSION OF A HIGH-SPEED JET BY WATER INJECTION, A PIV STUDY OF A CLOUD-LIKE FLOW, 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, UNSTEADY SEPARATION IN A FLARE INDUCED HYPERSONIC SHOCK-WAVE BOUNDARY-LAYER INTERACTION FLOWFIELD, 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, SUPPRESSION OF SELF-SUSTAINED OSCILLATIONS IN A SUPERSONIC IMPINGING JETS, FLOW AND ACOUSTIC PROPERTIES OF UNDEREXPANDED ELLIPTIC-SLOT JETS, A PIV STUDY OF SUPERSONIC IMPINGING JET, EXPERIMENTAL STUDY ON THE NOISE CHARACTERISTICS OF NOTCHED CIRCULAR-SLOT JETS, FLOW AND NOISE CHARACTERISTICS OF NOTCHED ELLIPTIC-ORIFICE JETS, EXPERIMENTS OF A PLUME WITH OFF-SOURCE HEATING, THE REDUCTION IN MINGLING WITH AMBIENT FLUID IN A JET WITH OFF-SOURCE HEATING, VISUALIZATION STUDIES OF CLOUD-LIKE FLOWS, DEVELOPMENTS OF A PLUME WITH OFF-SOURCE VOLUMETRIC HEATING, SUPERSONIC SEPARATION WITH OBSTRUCTIONS, EXPERIMENTAL INVESTIGATION OF LIFT AND DRAG CHARACTERISTICS OF A TYPICAL MAV UNDER PROPELLER INDUCED FLOW, EXPERIMENTAL INVESTIGATION OF LIFT AND DRAG CHARACTERISTICS OF A TYPICAL MAV UNDER PROPELLER INDUCED FLOW, TRANSITIONS IN TURBULENT ROTATING CONVECTION: A LAGRANGIAN PERSPECTIVE1, CORRELATION STUDIES IN THE ACOUSTIC FAR-FIELD OF NON-IDEALLY EXPANDED JETS1, CORRELATION STUDIES IN THE ACOUSTIC FAR-FIELD OF NON-IDEALLY EXPANDED JETS, CORRELATION STUDIES IN THE ACOUSTIC FAR-FIELD OF NON-IDEALLY EXPANDED JETS3

पत्रिका (89)

पेटेंट (4)

किताब (2)