Add to ORKGWind tunnel investigation for determination of subsonic and transonic aerodynamic characteristics of Saturn 1B launch vehicl
Transonic wind tunnel tests were run on a 0.015 scale model of the Space Shuttle Orbiter Vehicle in ...
Data reduction of transonic wind tunnel static pressure variation tests for correcting Saturn 5 dat
An experimental investigation of plume-induced flow separation on the National Launch System (NLS) 1...
Transonic wind pressure tunnel investigation for aerodynamic characteristics of Saturn IB APOLLO la...
The static stability and axial force characteristics of an upper stage Saturn 1B/Apollo model were i...
Wind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander con...
Aerodynamic hinge moments caused by external flow on saturn i, block i nozzle configuration
Effects of flow separation on aeroelastic characteristics of Saturn IB and Saturn V launch vehicles ...
Aerodynamic hinge moments for scale model boost stage nozzle of Saturn V launch vehicle during cold ...
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
Experimental static aerodynamic data for Apollo, Saturn 5 launch vehicle configuration
Aerodynamic damping and buffet response of aeroelastic model of Saturn I Block II LAUNCH vehicl
Shadowgraph study of upper stage flow fields of Saturn V launch vehicle configuration
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
A wind tunnel study to determine the supersonic aerodynamic characteristics of a 0.01925-scale model...
Transonic wind tunnel tests were run on a 0.015 scale model of the Space Shuttle Orbiter Vehicle in ...
Data reduction of transonic wind tunnel static pressure variation tests for correcting Saturn 5 dat
An experimental investigation of plume-induced flow separation on the National Launch System (NLS) 1...
Transonic wind pressure tunnel investigation for aerodynamic characteristics of Saturn IB APOLLO la...
The static stability and axial force characteristics of an upper stage Saturn 1B/Apollo model were i...
Wind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander con...
Aerodynamic hinge moments caused by external flow on saturn i, block i nozzle configuration
Effects of flow separation on aeroelastic characteristics of Saturn IB and Saturn V launch vehicles ...
Aerodynamic hinge moments for scale model boost stage nozzle of Saturn V launch vehicle during cold ...
A 1.75% scale force and moment model of the Space Launch System was tested in the NASA Langley Resea...
Experimental static aerodynamic data for Apollo, Saturn 5 launch vehicle configuration
Aerodynamic damping and buffet response of aeroelastic model of Saturn I Block II LAUNCH vehicl
Shadowgraph study of upper stage flow fields of Saturn V launch vehicle configuration
Wind tunnel study of aerodynamic characteristics of three scale model multistage launch vehicles at ...
A wind tunnel study to determine the supersonic aerodynamic characteristics of a 0.01925-scale model...
Transonic wind tunnel tests were run on a 0.015 scale model of the Space Shuttle Orbiter Vehicle in ...
Data reduction of transonic wind tunnel static pressure variation tests for correcting Saturn 5 dat
An experimental investigation of plume-induced flow separation on the National Launch System (NLS) 1...