41st AIAA Fluid Dynamics Conference and Exhibit
Latest Publications

TOTAL DOCUMENTS

204

(FIVE YEARS 0)

H-INDEX

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781600869471

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Feedback Control of Airfoil Lift using Dense Surface Sensors and Reduced Order Models

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3115 ◽

2011 ◽

Cited By ~ 2

Author(s):

Jurgen Seidel ◽

Casey Fagley ◽

Thomas McLaughlin

Keyword(s):

Feedback Control ◽

Reduced Order Models ◽

Reduced Order

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Numerical Modeling of Multiphase, Multi-Material Blast/Structure Interactions

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3722 ◽

2011 ◽

Cited By ~ 1

Author(s):

Joseph Baum ◽

Orlando Soto ◽

Fumiya Togashi ◽

Rainald Lohner

Keyword(s):

Numerical Modeling

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Numerical Simulations of Transition Experiments in the Hypersonic Ballistic Range

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3416 ◽

2011 ◽

Cited By ~ 1

Author(s):

Seokkwan Yoon ◽

Michael Barnhardt ◽

Emre Sozer ◽

Graham Candler

Keyword(s):

Numerical Simulations ◽

Ballistic Range

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Numerical Simulation of Nose Bluntness Effects on Hypersonic Boundary Layer Receptivity to Freestream Disturbances

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3079 ◽

2011 ◽

Cited By ~ 3

Author(s):

Xiaolin Zhong ◽

Jia Lei

Keyword(s):

Numerical Simulation ◽

Boundary Layer ◽

Hypersonic Boundary Layer

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PLIF Study of Mars Science Laboratory Capsule Reaction Control System Jets

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3890 ◽

2011 ◽

Cited By ~ 4

Author(s):

Craig Johansen ◽

Paul Danehy ◽

Scott Ashcraft ◽

Brett Bathel ◽

Jennifer Inman ◽

...

Keyword(s):

Control System ◽

Science Laboratory ◽

Mars Science Laboratory ◽

Reaction Control System

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Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3257 ◽

2011 ◽

Cited By ~ 2

Author(s):

Brandon Pruski ◽

Raymond Humble ◽

Rodney Bowersox

Keyword(s):

Flow Structure ◽

Leading Edge ◽

Naca 0012 ◽

Edge Flow

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An Experimental Investigation on the Trailing Edge Cooling of Turbine Blades by using PIV and PSP Techniques

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3269 ◽

2011 ◽

Author(s):

Hui Hu ◽

Zifeng Yang

Keyword(s):

Experimental Investigation ◽

Turbine Blades ◽

Trailing Edge

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Direct Numerical Simulation of Transonic Wake Propagation in the Presence of an Adverse Pressure Gradient and Streamline Curvature

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3091 ◽

2011 ◽

Author(s):

Jeffrey Gibson ◽

Steven Gorrell

Keyword(s):

Numerical Simulation ◽

Direct Numerical Simulation ◽

Pressure Gradient ◽

Adverse Pressure Gradient ◽

Streamline Curvature

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Mono-Dispersed Water Droplet Delivery in a Small-Scale Refrigerated Wind Tunnel

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3274 ◽

2011 ◽

Cited By ~ 1

Author(s):

Kyle Hutchings ◽

David Thompson ◽

Stefan Jung ◽

Dominik Raps

Keyword(s):

Wind Tunnel ◽

Water Droplet ◽

Small Scale

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Experimental and Theoretical Study of Attitude Control of Flapping Wing Micro Aerial Vehicle

41st AIAA Fluid Dynamics Conference and Exhibit ◽

10.2514/6.2011-3253 ◽

2011 ◽

Cited By ~ 1

Author(s):

Koji Isogai ◽

Hiroyasu Kawabe ◽

Hiroto Nagai ◽

Shun Nishiguchi

Keyword(s):

Attitude Control ◽

Theoretical Study ◽

Flapping Wing ◽

Micro Aerial Vehicle ◽

Aerial Vehicle

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41st AIAA Fluid Dynamics Conference and ExhibitLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Feedback Control of Airfoil Lift using Dense Surface Sensors and Reduced Order Models

Numerical Modeling of Multiphase, Multi-Material Blast/Structure Interactions

Numerical Simulations of Transition Experiments in the Hypersonic Ballistic Range

Numerical Simulation of Nose Bluntness Effects on Hypersonic Boundary Layer Receptivity to Freestream Disturbances

PLIF Study of Mars Science Laboratory Capsule Reaction Control System Jets

Leading Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil

An Experimental Investigation on the Trailing Edge Cooling of Turbine Blades by using PIV and PSP Techniques

Direct Numerical Simulation of Transonic Wake Propagation in the Presence of an Adverse Pressure Gradient and Streamline Curvature

Mono-Dispersed Water Droplet Delivery in a Small-Scale Refrigerated Wind Tunnel

Experimental and Theoretical Study of Attitude Control of Flapping Wing Micro Aerial Vehicle

41st AIAA Fluid Dynamics Conference and Exhibit
Latest Publications