English
English
Hindi
Contact Us
Home
>
Publication
>
Flow Investigation of Linear Cluster Plug Nozzle
Flow Investigation of Linear Cluster Plug Nozzle
Send E-Mail
Flow Investigation of Linear Cluster Plug Nozzle
Flow Investigation of Linear Cluster Plug Nozzle,” Journal of spacecraft and rockets, Vol. 53, No. 1, Jan–Feb 2016, pp 39-45.
X
Contact Form
First Name
University/Organization
E-Mail
Phone
Message
Captcha
Send
DHVANI- An Indigenous Advanced Target Training System
Preliminary noise analysis of the Indigenous Wankel Rotary Combustion Engine
Shock wave Boundary layer interaction in supersonic flow over a forward-facing step
Influence of Base Cavity on Base Pressure at Subsonic and Supersonic Mach Numbers
An Experimental Study on Shock Wave Boundary Layer Interaction over a Forward-Facing Step
Effect of Modification of Sharp Base on Base Pressure
Effect of Step Height on Flow Separation in Supersonic Flow
Supersonic Flow Separation in Front of a Forward-Facing Step
Experimental Study of Supersonic Flow over a Compression Corner
Base Heat Transfer Studies of a Blunt Body at Hypersonic Number
Effect of Transonic Fresstream on Linear Cluster Plug Nozzle Flow
Near Wake Field of Circular Cylinder With a Forward Splitter Plate
Effect of Clustering on Linear Plug Nozzle Flow Field for Overexpanded Internal Jet
Analysis of annular plug nozzle flowfied,” Journal of spacecraft and rockets
Flowfield analysis of linear plug nozzle
Study of Cluster Linear Plug Nozzle Flow Field in Freestream Flow
Wake of Circular Cylinder with Forward Splitter Plate
Flow past a circular cylinder with forward splitter plate
Cluster Plug Nozzle Flow Field
Self-Activated Movable Flaps on Low Aspect Ratio Wings at Low Reynolds Numbers
Aerodynamic Analysis of Annular Plug Nozzles
Experiments on a Flying Wing Configuration for Code Validation
Experimental Investigation of Lift and Drag Characteristics of a Typical MAV under Propeller Induced Flow
Flowfield Analysis of Truncated and Clustered Linear Plug Nozzles
Experimental Analysis of Linear Plug Nozzle
Computational and Experimental Analysis of Linear Plug Nozzle
Experimental Study of Supersonic Flow over a Forward Facing Step
Influence of leading edge tubercles on aerodynamic characteristics of a high aspect-ratio UAV
Acoustic characterization of jet interaction with launch structures during lift-off
Influence of propeller slipstream on vortex flow field over a typical micro air vehicle
Non-Intrusive flow diagnostics for aerospace applications
Studies on the Influence of Steady Microactuators on Shock-Wave/Boundary-Layer Interaction
Effect of Truncation on the Aeroacoustics of an Annular Aerospike Nozzle’
Density Field Visualization of a Micro-Explosion Using Background Oriented Schlieren
Role of coherent structures in supersonic impinging jets
Supersonic Testing of NAL Binary Pressure Sensitive Paint
Experimental Studies on a Rudimentary Four Wheel Landing Gea
Generation and Control of Oblique Shocks Using Microjets
New Approaches for Analysis of Jet Noise Data
Application of Photogrammetry to Surface Flow Visualization
Experimental Studies of Propeller Induced Flow over a Typical Micro Air Vehicle
Density Field Measurements of a Supersonic Impinging Jet with Microjet Control
Experimental study on a jet issuing from an elliptic nozzle with cylindrical tabs
Study of intermittent transitional boundary layer using PIV
Three-dimensional Tomographic Reconstruction of Density Field in an Afterbody Flow with Shock and Jet Effects
Resection Methodology for PSP Data Processing: Recent experiences in NAL
Pressure Sensitive Paint Measurements on a Delta Wing in Supersonic Flow
Forward Flight Effects on Fan Noise from Supersonic 2-D Inlets
PIV Studies of Large Scale Structures in the Near Field of Small Aspect Ratio Elliptic Jets
Investigation of hysteresis effects on a wing-flap configuration at high-lift using PIV
Density Measurements in an Axisymmetric Underexpanded Jet Using Background Oriented Schlieren Technique
A comparative Study of Different PSP image Registration Techniques
Density Measurements using Background Oriented Schlieren Technique
Turbulence and Noise Suppression of a high-speed jet by Water Injection
Experimental Studies on a Lambda Wing Configuration for CFD Code Validation
A PIV study of a cloud-like flow
Suppression of Self-Sustained Oscillations in a Supersonic Impinging Jets
A PIV study of supersonic impinging jet
The reduction in mingling with ambient fluid in a jet with off-source heating
Experiments of a plume with off-source heating
Visualization studies of cloud-like flows
Developments of a plume with off-source volumetric heating
Computational Studies on Flow through De Laval Nozzle
Shockwave/boundary-layer interaction control on a compression ramp using steady microjets
Control of shock unsteadiness in shock boundary-layer interaction on a compression corner using mechanical vortex generators
Control of Shock-Wave Boundary Layer interaction Using Steady Micro-Jets
Transition control of Mach to regular reflection induced interaction using an array of micro ramp vane-type vortex generators
Effect of Spike Truncation on the Acoustic Behavior of Annular Aerospike Nozzles
Control of base pressure for a boat-tailed axisymmetric afterbody via base geometry modifications
Experimental Studies on a Propelled Micro Air Vehicle
Assessment of Various Low-Profile Mechanical Vortex Generators in Controlling a Shock-Induced Separation”
Shock-wave boundary-layer interaction study on a compression corner using pressure-sensitive paint
Shock-Wave Boundary-Layer Interaction Control on a Compression Corner Using Mechanical Vortex Generators
Investigation of starting process of a movable intake configuration at high supersonic speeds
arametric Study on Steady Micro-Jet Actuators for Control of Unsteady Shock Motion in a compression induced interacton at Mach 2
Effect of differential sweep on a three dimensional sidewall type intake at Mach 3.5
Effect of Differential Sweep on a Three-Dimensional Sidewall-Type Intake at Mach 3.5
Studies on Three-Dimensional Intake with Bleed at M∞= 3.5
Control of Incident Shock Induced Separation at Mach 3.5 using an Array of Steady Micro-Jet Actuators
Experimental investigation on the near flow field of dual stream nozzles
Effect of mean and fluctuating pressure gradients on boundary layer turbulence
Identification of emergent motion compartments in the amniote embryo"
Transitions in turbulent rotating convection: A Lagrangian perspective
Flow anisotropy in rotating buoyancy-driven turbulence
Effect of particle injection on heat transfer in rotating Rayleigh ̶ Bénard convection
Heat transfer in rotating Rayleigh ̶ Bénard convection with rough plates
Effects of Fluctuating Pressure Gradients on Boundary Layer Turbulence
Modification of Turbulence in Boundary Layers by Mean and Fluctuating Pressure Gradients
Self-Adaptive Flaps on Low Aspect Ratio Wings at Low Reynolds Numbers
Turbulence in Accelerating Boundary Layers
Correlation Studies in the Acoustic Far-Field of Non-ideally Expanded Supersonic Jets
Experimental Investigation of Turbulent Boundary Layers under Favorable Pressure Gradient
Unsteady Flow Field Downstream of a Sudden Expansion
Experimental Investigation of an Incident Shock-Induced Interaction near an Expansion Corner
Prediction of Launch Vehicle Noise during Lift-off using a Modified Eldred’s Method
Effect of Inverted Triangular Tabs on Mitigation of Jet Noise from Axisymmetric Convergent Nozzles
Turbulence suppression of low Reynolds number circular jet using Dielectric Barrier Discharge plasma actuators
Empirical Evaluation of Wall Interference Effects on a Laminar Supercritical Airfoil at Transonic Speeds
Testing of indegenously developed pressure sensitive paint for wind tunnel studies
Supersonic Testing of NAL Binary Pressure Sensitive Paint
An overview of Intake Model Studies Carried out at 0.3 m Trisonic Wind Tunnel
Aerodynamic Performance Evaluation Of Twinjet Afterbody Using Flow Through Balance
Experimental investigation of a Mach 4 shock-wave turbulent boundary layer interaction near an expansion corner
Experimental Investigation of Sharp Fin induced Shock Wave Boundary Layer Interaction
Three Dimensional Interaction Flow Field in a Supersonic Inlet like Configuration
Control of low speed cavity flow using streamwise tabs at leading edge
Supersonic Separation with Obstructions
Flow and Noise Characteristics of Notched Elliptic-Orifice Jets
Experimental Study on the Noise Characteristics of Notched Circular-Slot Jets
Flow and Acoustic Properties of Underexpanded Elliptic-Slot Jets
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
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
Relation Between Shock Unsteadiness and the Origin of Side-Loads in a Thrust Optimized Parabolic Rocket Nozzle
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
Study on Restricted Shock Separation Phenomena in a Thrust Optimized Parabolic (TOP) Nozzle
Flow Separation Characteristics of Overexpanded Nozzles
Studies on an Elliptic Jet with Cylindrical tabs’
StFlow Separation Characteristics of a Dual-Bell Nozzle during its Transition Modes
Study of Jets from Rectangular Nozzles with Square Grooves’
Unsteady Shock Motions in an Over-Expanded Parabolic Rocket Nozzle
Experimental study of unsteady wake effect on a film-cooled pitchwise-curved surface
Unsteady Flow Conditions During Dual-Bell Sneak Transition
Numerical Simulation of Shock/Boundary Layer Interaction in Supersonic Overexpanded Nozzles
Experimental Study of Subsonic and Sonic Jets Controlled by Air Tabs
Editorial on the Thematic Issue: Supersonic Flow Control, Shock Waves
Experimental and numerical study of secondary flow and coolant film interaction in a high subsonic cascade Tunnel
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
Gas Density Effects on Dual-Bell Transition Behavior
Reynolds Number Influence on Dual-Bell Transition Phenomena
Experimental Studies on Rectangular Jets with Trapezoidal Tabs
Effect of Ambient Pressure Fluctuations on Dual-Bell Transition Behavior
Experimental study on NACA4415 airfoil at low Reynolds number
Effect of leading edge tubercles on flow field over naca-4415 airfoil at low Reynolds number
Experimental studies on the effect of leading edge tubercles on laminar separation bubble
Experimental studies on SM-4308 airfoil at low Reynolds number
Experimental Studies of Flow Field and Aeroacoustic characteristics of a Dual Stream Bevelled Nozzle
Aerodynamic characteristics of Eppler 61 airfoil at Low Reynolds numbers
Background Oriented Schlieren based Mixing enhancement studies in free-jets from supersonic ESTS lobed nozzles
High Speed Visualization of blast waves emerging from a small-scale combustion driven cloud
Dielectric barrier discharge for aerodynamic flow control
PIV investigation on the Lift Enhancing Capabilities of Self-Adaptive Flaps on Low Aspect Ratio Wings
Transitions in turbulent rotating convection: A Lagrangian perspective1
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
Correlation Studies in the Acoustic Far-Field of Non-ideally Expanded Jets
Correlation Studies in the Acoustic Far-Field of Non-ideally Expanded Jets1
Correlation Studies in the Acoustic Far-Field of Non-ideally Expanded Jets3
Facebook
Twitter
Youtube
Google Plus
Instagram
Archives of NAL
Technology
Facilities
Techniques
Divisions
Research
Publication
Business
Services
Last updated on : 13-10-2017 03:17:41pm
English
Hindi