30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Latest Publications

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Published By American Institute Of Aeronautics And Astronautics

9781624102875

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Molecular Rayleigh scattering to measure fluctuations in density and temperature in low speed heated wind tunnel flows

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2529 ◽

2014 ◽

Cited By ~ 2

Author(s):

Jayanta Panda ◽

Stephen Schery

Keyword(s):

Wind Tunnel ◽

Rayleigh Scattering ◽

Low Speed

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A Study of Potential Test Capabilities of the NASA Langley 0.3-Meter Transonic Cryogenic Wind Tunnel

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2654 ◽

2014 ◽

Author(s):

Ben D. Phillips ◽

Colin P. Britcher

Keyword(s):

Wind Tunnel ◽

Cryogenic Wind Tunnel ◽

Potential Test

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Characterization of the NASA Langley Arc Heated Scramjet Test Facility using NO PLIF

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2652 ◽

2014 ◽

Cited By ~ 4

Author(s):

Forrest G. Kidd ◽

Venkateswaran Narayanaswamy ◽

Paul M. Danehy ◽

Jennifer A. Inman ◽

Brett F. Bathel ◽

...

Keyword(s):

Test Facility

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2-D Velocity and Vorticity Measurements with FLEET

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2229 ◽

2014 ◽

Cited By ~ 3

Author(s):

Nathan D. Calvert ◽

Arthur Dogariu ◽

Richard B. Miles

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Diagnosis of High Speed Flows using Filtered Rayleigh Scattering

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2231 ◽

2014 ◽

Cited By ~ 7

Author(s):

Jacob George ◽

Tom P. Jenkins ◽

Richard B. Miles

Keyword(s):

High Speed ◽

Rayleigh Scattering ◽

High Speed Flows

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Application of a Novel Projection Focusing Schlieren System in NASA Test Facilities

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2522 ◽

2014 ◽

Cited By ~ 5

Author(s):

Amy F. Fagan ◽

Drew L'Esperance ◽

Khairul Q. Zaman

Keyword(s):

Schlieren System

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Mach Number Control improvement in ONERA S1MA large Transonic Wind Tunnel

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2108 ◽

2014 ◽

Cited By ~ 3

Author(s):

Pascal Crozier ◽

Christian Chargy ◽

Robert Pichon

Keyword(s):

Mach Number ◽

Wind Tunnel ◽

Transonic Wind Tunnel

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Development and Feasibility of a Non-Invasive, Wireless Parachute Load Distribution Measuring System

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2799 ◽

2014 ◽

Cited By ~ 1

Author(s):

Travis Fields

Keyword(s):

Load Distribution ◽

Measuring System ◽

Non Invasive

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Large-Span, Non-Contact Surface Profilometry for Laminar-Flow Diagnostics

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2940 ◽

2014 ◽

Cited By ~ 3

Author(s):

Brian K. Crawford ◽

Glen T. Duncan ◽

David E. West ◽

William S. Saric

Keyword(s):

Laminar Flow ◽

Contact Surface ◽

Flow Diagnostics ◽

Large Span ◽

Surface Profilometry

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A New Global Regression Analysis Method for the Prediction of Wind Tunnel Model Weight Corrections

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2014-2797 ◽

2014 ◽

Author(s):

Norbert M. Ulbrich ◽

Max Amaya ◽

Thomas Bridge

Keyword(s):

Regression Analysis ◽

Wind Tunnel ◽

Analysis Method ◽

Wind Tunnel Model ◽

Tunnel Model ◽

Global Regression ◽

Model Weight

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30th AIAA Aerodynamic Measurement Technology and Ground Testing ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Molecular Rayleigh scattering to measure fluctuations in density and temperature in low speed heated wind tunnel flows

A Study of Potential Test Capabilities of the NASA Langley 0.3-Meter Transonic Cryogenic Wind Tunnel

Characterization of the NASA Langley Arc Heated Scramjet Test Facility using NO PLIF

2-D Velocity and Vorticity Measurements with FLEET

Diagnosis of High Speed Flows using Filtered Rayleigh Scattering

Application of a Novel Projection Focusing Schlieren System in NASA Test Facilities

Mach Number Control improvement in ONERA S1MA large Transonic Wind Tunnel

Development and Feasibility of a Non-Invasive, Wireless Parachute Load Distribution Measuring System

Large-Span, Non-Contact Surface Profilometry for Laminar-Flow Diagnostics

A New Global Regression Analysis Method for the Prediction of Wind Tunnel Model Weight Corrections

30th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Latest Publications