22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Latest Publications

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Published By American Institute Of Aeronautics And Astronautics

9781624101120

Latest Documents Most Cited Documents Contributed Authors Related Sources Related Keywords

Point Doppler Velocimeter (pDv) Jet Data Using Avalanche Photodiodes (APDs)

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3229 ◽

2002 ◽

Author(s):

John Kuhlman ◽

Tom Scarberry

Keyword(s):

Avalanche Photodiodes

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An Overview of Advanced Propeller Simulation Tests in the German Dutch Wind Tunnels (DNW)

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-2920 ◽

2002 ◽

Cited By ~ 7

Author(s):

Iwan Philipsen ◽

Harrie Hoeijmakers ◽

Sinus Hegen

Keyword(s):

Wind Tunnels

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Progress in the Operation of the Boeing/AFOSR Mach-6 Quiet Tunnel

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3033 ◽

2002 ◽

Cited By ~ 6

Author(s):

Steven Schneider ◽

Shin Matsumura ◽

Shann Rufer ◽

Craig Skoch ◽

Erick Swanson

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Development of an Effective Technology for Gas Turbine Engine Performance Testing

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3047 ◽

2002 ◽

Author(s):

Inyoung Yang ◽

Yongmin Jun ◽

Chuntaek Kim ◽

Sooseok Yang ◽

Daesung Lee

Keyword(s):

Gas Turbine ◽

Engine Performance ◽

Performance Testing ◽

Gas Turbine Engine ◽

Turbine Engine ◽

Effective Technology

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Mars Entry Simulation with Dust Using an Inductively Heated Generator

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3237 ◽

2002 ◽

Cited By ~ 4

Author(s):

Pia Endlich ◽

Monika Auweter-Kurtz ◽

Georg Herdrich ◽

Stefan Laure

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Rotatable Single-Hole Pressure Probe for Flow Velocity and Direction

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3138 ◽

2002 ◽

Cited By ~ 3

Author(s):

Russell Westphal ◽

Martin Prather ◽

Michael Toyooka

Keyword(s):

Flow Velocity ◽

Pressure Probe ◽

Hole Pressure ◽

Single Hole

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A 2-Liter, 2000 MPa Air Source for the Radiatively Driven Hypersonic Wind Tunnel (Invited)

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3127 ◽

2002 ◽

Cited By ~ 2

Author(s):

Marc Costantino ◽

Dave Lofftus ◽

Larry Hunter

Keyword(s):

Wind Tunnel ◽

Hypersonic Wind Tunnel

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A Review of Standards Model Testing in the Boeing Transonic Wind Tunnel (Invited)

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-2789 ◽

2002 ◽

Cited By ~ 2

Author(s):

Dale Belter ◽

Kevin Mejia

Keyword(s):

Wind Tunnel ◽

Model Testing ◽

Transonic Wind Tunnel

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Time-Sequenced PIV Imaging of a Shock/Boundary Layer Interaction

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3232 ◽

2002 ◽

Cited By ~ 1

Author(s):

Noel Clemens ◽

Y Hou ◽

David Dolling

Keyword(s):

Boundary Layer ◽

Layer Interaction ◽

Shock Boundary Layer Interaction ◽

Boundary Layer Interaction

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Development and Ground Testing of Heat Flux Gages for High Enthalpy Supersonic Flight Tests

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference ◽

10.2514/6.2002-3133 ◽

2002 ◽

Cited By ~ 2

Author(s):

Theodore Smith ◽

Greg Walker ◽

Joseph Schetz

Keyword(s):

Heat Flux ◽

Flight Tests ◽

Supersonic Flight ◽

Ground Testing ◽

High Enthalpy

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22nd AIAA Aerodynamic Measurement Technology and Ground Testing ConferenceLatest Publications

TOTAL DOCUMENTS

H-INDEX

Published By American Institute Of Aeronautics And Astronautics

Point Doppler Velocimeter (pDv) Jet Data Using Avalanche Photodiodes (APDs)

An Overview of Advanced Propeller Simulation Tests in the German Dutch Wind Tunnels (DNW)

Progress in the Operation of the Boeing/AFOSR Mach-6 Quiet Tunnel

Development of an Effective Technology for Gas Turbine Engine Performance Testing

Mars Entry Simulation with Dust Using an Inductively Heated Generator

Rotatable Single-Hole Pressure Probe for Flow Velocity and Direction

A 2-Liter, 2000 MPa Air Source for the Radiatively Driven Hypersonic Wind Tunnel (Invited)

A Review of Standards Model Testing in the Boeing Transonic Wind Tunnel (Invited)

Time-Sequenced PIV Imaging of a Shock/Boundary Layer Interaction

Development and Ground Testing of Heat Flux Gages for High Enthalpy Supersonic Flight Tests

22nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Latest Publications