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Common Research Wind Tunnel Model
Common Research Wind Tunnel Model

Obtain aerodynamic and flow visualization data on a generic transport model to assess the performance of computational fluid dynamics (CFD)…

Common Research Wind Tunnel Model
Common Research Wind Tunnel Model

Obtain aerodynamic and flow visualization data on a generic transport model to assess the performance of computational fluid dynamics (CFD)…

Common Research Wind Tunnel Model with a Particle Image Velocimetry Plane
Common Research Wind Tunnel Model with a Particle Image Velocimetry Plane

To obtain aerodynamic and flow visualization data on a generic transport model to assess the performance of computational fluid dynamics…

Common Research Model Test Crew
Common Research Model Test Crew

Obtain aerodynamic and flow visualization data on a generic transport model to assess the performance of computational fluid dynamics (CFD)…

2.8% Ares 1 Acoustic Reentry Wind Tunnel Model
2.8% Ares 1 Acoustic Reentry Wind Tunnel Model

Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry…

2.8% Ares I Acoustic Reentry Wind Tunnel Model
2.8% Ares I Acoustic Reentry Wind Tunnel Model

Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry…

Facility Aerodynamics Validations and Operations Research Model
Facility Aerodynamics Validations and Operations Research Model

Cooperative wind tunnel tests to provide engineering insight into facility processes, data reduction, flow quality and a comparative data assessment.

Facility Aerodynamics Validations and Operations Research Model Test Crew
Facility Aerodynamics Validations and Operations Research Model Test Crew

Cooperative wind tunnel tests to provide engineering insight into facility processes, data reduction, flow quality and a comparative data assessment.

6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module
6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module

Test to obtain acoustic data on jet interactions of plume simulations with separation aerodynamic effects for selected specific conditions.

6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module
6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module

Test to obtain acoustic data on jet interactions of plume simulations with separation aerodynamic effects for selected specific conditions.