NASA Ames Unitary Plan Wind TunnelAerial View of the Unitary Plan Wind Tunnel at NASA AmesSpace Launch System (SLS) installed in the 11-by 11-foot test section.NASA Ames Research Center Check Standard Model installed in the 11-by 11-Foot Transonic Wind Tunnel.Sierra Nevada Corporation, or SNC, DREAM Chaser lifting body spaceplane in the NASA Ames 9x7-foot Supersonic Wind Tunnel, or SWT.Space Launch System (SLS) ModelThe Subsonic Ultra Green Aircraft Research (SUGAR) Project is a multiphase, collaborative research project conducted by NASA and Boeing Research...Ultra High Bypass (UHB) Nacelle Semi Span Model. To test Force, moment, and pressure data measurements of the aerodynamic effects...Obtain aerodynamic and flow visualization data on a generic transport model to assess the performance of computational fluid dynamics (CFD)...Low boom passenger airline concept to obtain force and pressure measurements and calibrate computational fluid dynamics (CFD) tools estimates.Ultra-High Bypass (UHB) Semi-Span Model in the Unitary Plan Wind Tunnel 11-by 11-foot Test Section. The model is the latest...The Subsonic Ultra Green Aircraft Research (SUGAR) Project is a multiphase, collaborative research project conducted by NASA and Boeing Research...The Subsonic Ultra Green Aircraft Research (SUGAR) Project is a multiphase, collaborative research project conducted by NASA and Boeing Research...Test provided measurements of the aeroacoustics of the Orion Launch Abort Vehicle (LAV) configuration. Hot helium was used to simulate...Common Research Wind Tunnel Model used to obtain aerodynamic and flow visualization data on a generic transport model to assess...Common Research Wind Tunnel Model used to obtain aerodynamic and flow visualization data on a generic transport model to assess...Common Research Wind Tunnel Model used to obtain aerodynamic and flow visualization data on a generic transport model to assess...Common Research Wind Tunnel Model used to obtain aerodynamic and flow visualization data on a generic transport model to assess...Common Research Model (CRM) Test t-11-0216 in the NASA Ames 11x11_foot Transonic Wind Tunnel with PIV laser sheet over model....Common Research Wind Tunnel Model Test Crew. Common Research Wind Tunnel Model used to obtain aerodynamic and flow visualization data...Modified 6% Crew Exploration Vehicle (CEV) Alternate Launch Abort System (ALAS) ConfigurationTest to investigate aerodynamic proximity and jettison motor plume interaction effects on the separation of the crew module from the...Ames Low Boom Wing Tail Model in the Unitary Plan Wind Tunnel 9-by 7-foot test section. Test to refine sonic...Low boom passenger airline concept to obtain force and pressure measurements and calibrate computational fluid dynamics (CFD) tools estimates.Tri-jet supersonic transport low-boom model 1044 mounted in Ames 9-by 7-toot supersonic wind tunnel for measurement of sonic boom and...Wind tunnel test to calibrate the flow-around balance model assembly for momentum corrections.SNC Dream Chaser Lifting Body Model. Sierra Nevada Corporation, or SNC, DREAM Chaser lifting body spaceplane in the NASA Ames...Sierra Nevada Corporation, or SNC, Dream Chaser lifting body spaceplane in the NASA Ames 11x11-foot Transonic Wind Tunnel, or TWT.Test to determine fluctuating pressure environments from a 2.8% scale Ares I first stage configuration to verify and update reentry...2.8% Ares 1 Acoustic Reentry Wind Tunnel Model Test to determine fluctuating pressure environments from a 2.8% scale Ares I...6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module. Test to obtain acoustic data on jet interactions of...6% Crew Exploration Vehicle/ Launch Abort Vehicle and Encapsulated Service Module. Test to obtain acoustic data on jet interactions of...The Facility Aerodynamics Validation and Operational Research (FAVOR) model, mounted in the Ames Research Center 11- by 11-Foot Unitary Plan...Facility Aerodynamics Validations and Operations Research Model Test Crew.3% Space Shuttle Aero Acoustics Wind Tunnel Model3% Space Shuttle Aero Acoustics Wind Tunnel Model.NASA Ames Research Center Check Standard Model installed in the 11-by 11-Foot Transonic Wind Tunnel.Ultra-High Bypass (UHB) Semi-Span Model in the Unitary Plan Wind Tunnel 11-by 11-foot Test Section. The model is the latest...