34th AIAA Applied Aerodynamics Conference
Latest Publications

TOTAL DOCUMENTS

167

(FIVE YEARS 0)

H-INDEX

(FIVE YEARS 0)

Published By American Institute Of Aeronautics And Astronautics

9781624104374

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Hypersonic Experimental Aero-thermal Capability Study through Multilevel Fidelity Computational Fluid Dynamics

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-3577 ◽

2016 ◽

Author(s):

Denton G. Sagerman ◽

James Tancred ◽

Markus Rumpfkeil ◽

Barry M. Hellman

Keyword(s):

Fluid Dynamics ◽

Computational Fluid Dynamics

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Numerical investigations of the vortical flow on swept wings with round leading edges

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-4172 ◽

2016 ◽

Cited By ~ 1

Author(s):

Andreas Schuette

Keyword(s):

Vortical Flow ◽

Numerical Investigations ◽

Leading Edges ◽

Swept Wings

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Passive flow control study in a convoluted intake using Stereo Particle Image Velocimetry

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-3563 ◽

2016 ◽

Cited By ~ 2

Author(s):

Geoffrey Tanguy ◽

Pavlos Zachos ◽

David G. MacManus ◽

Daniel Gil-Prieto ◽

Eric Garnier

Keyword(s):

Particle Image Velocimetry ◽

Flow Control ◽

Particle Image ◽

Passive Flow Control ◽

Passive Flow ◽

Image Velocimetry ◽

Stereo Particle Image Velocimetry ◽

Control Study

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Design and Analyses of High Aspect Ratio Nozzles for Distributed Propulsion Acoustic Measurements

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-3876 ◽

2016 ◽

Author(s):

Vance F. Dippold

Keyword(s):

Aspect Ratio ◽

High Aspect Ratio ◽

Acoustic Measurements ◽

Distributed Propulsion

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Nonlinear Lifting-Line Algorithm for Unsteady and Post-stall Conditions

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-4164 ◽

2016 ◽

Cited By ~ 3

Author(s):

Joaquim N. Dias

Keyword(s):

Lifting Line

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Numerical Investigation of Vortex Breakdown

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-4174 ◽

2016 ◽

Author(s):

Tjarke van Jindelt ◽

Jan Willem van der Burg ◽

Edwin T. van der Weide ◽

Harry W. Hoeijmakers

Keyword(s):

Numerical Investigation ◽

Vortex Breakdown

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Convoluted Intake Distortion Measurements Using Stereo Particle Image Velocimetry

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-3560 ◽

2016 ◽

Cited By ~ 6

Author(s):

Daniel Gil-Prieto ◽

Pavlos Zachos ◽

David G. MacManus ◽

Geoffrey Tanguy

Keyword(s):

Particle Image Velocimetry ◽

Particle Image ◽

Image Velocimetry ◽

Stereo Particle Image Velocimetry

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Investigation of Unsteady Characteristics of Vortex Breakdown

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-4175 ◽

2016 ◽

Author(s):

Lan Chen ◽

Jinjun Wang ◽

Lihao Feng ◽

Handong Hu

Keyword(s):

Vortex Breakdown ◽

Unsteady Characteristics

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Aerodynamic Modeling of Transonic Aircraft Using Vortex Lattice Coupled with Transonic Small Disturbance for Conceptual Design

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-3418 ◽

2016 ◽

Cited By ~ 15

Author(s):

Daniel Chaparro ◽

Gustavo E. Fujiwara ◽

Eric Ting ◽

Nhan T. Nguyen

Keyword(s):

Conceptual Design ◽

Vortex Lattice ◽

Small Disturbance ◽

Aerodynamic Modeling

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Effects of Leading-Edge Structures on Stall Behaviors of a NACA0015 Airfoil: A Multi-plane PIV Study

34th AIAA Applied Aerodynamics Conference ◽

10.2514/6.2016-3732 ◽

2016 ◽

Cited By ~ 2

Author(s):

Yan Zhang ◽

Jordi Estevadeordal ◽

Sadhana Bhusal ◽

Jesstin Krech

Keyword(s):

Leading Edge

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34th AIAA Applied Aerodynamics ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Hypersonic Experimental Aero-thermal Capability Study through Multilevel Fidelity Computational Fluid Dynamics

Numerical investigations of the vortical flow on swept wings with round leading edges

Passive flow control study in a convoluted intake using Stereo Particle Image Velocimetry

Design and Analyses of High Aspect Ratio Nozzles for Distributed Propulsion Acoustic Measurements

Nonlinear Lifting-Line Algorithm for Unsteady and Post-stall Conditions

Numerical Investigation of Vortex Breakdown

Convoluted Intake Distortion Measurements Using Stereo Particle Image Velocimetry

Investigation of Unsteady Characteristics of Vortex Breakdown

Aerodynamic Modeling of Transonic Aircraft Using Vortex Lattice Coupled with Transonic Small Disturbance for Conceptual Design

Effects of Leading-Edge Structures on Stall Behaviors of a NACA0015 Airfoil: A Multi-plane PIV Study

34th AIAA Applied Aerodynamics Conference
Latest Publications