Add to ORKGWind tunnel tests to determine aerodynamic characteristics of Viking spacecraft entry and lander configurations at transonic spee
Tests of the Viking 16.15-meter nominal-diameter disk-gap-band parachute were conducted at Mach numb...
Results are presented for wind tunnel tests of a one to twelve scale model of the M2-F2 lifting body...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Six experimental investigations conducted in the transonic dynamics tunnel, which supported elements...
Longitudinal aerodynamic characteristics of Viking lander spacecraft at hypersonic spee
Comparisons are made between the LAURA Navier-Stokes code and Viking Lander Capsule hypersonic aerod...
An investigation was conducted to obtain flow properties in the wake of a preliminary configuration ...
An investigation was conducted to obtain flow properties in the wake of the Viking '75 entry vehicle...
The flow properties in the wake of 120 degree and 140 degree included angle cones and a model of the...
Results of an investigation to determine the full scale drag coefficient in the high speed, low dens...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
Wind tunnel investigation for determination of subsonic and transonic aerodynamic characteristics of...
A wind tunnel study to determine the supersonic aerodynamic characteristics of a 0.01925-scale model...
Flight qualifications for parachutes were tested on full-scale simulated Viking spacecraft at entry ...
Force tests of a model of a proposed six-engine hull-type seaplane were performed in the Langley 8-f...
Tests of the Viking 16.15-meter nominal-diameter disk-gap-band parachute were conducted at Mach numb...
Results are presented for wind tunnel tests of a one to twelve scale model of the M2-F2 lifting body...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration
Six experimental investigations conducted in the transonic dynamics tunnel, which supported elements...
Longitudinal aerodynamic characteristics of Viking lander spacecraft at hypersonic spee
Comparisons are made between the LAURA Navier-Stokes code and Viking Lander Capsule hypersonic aerod...
An investigation was conducted to obtain flow properties in the wake of a preliminary configuration ...
An investigation was conducted to obtain flow properties in the wake of the Viking '75 entry vehicle...
The flow properties in the wake of 120 degree and 140 degree included angle cones and a model of the...
Results of an investigation to determine the full scale drag coefficient in the high speed, low dens...
The performance of the Viking lander has been evaluated by using a Monte Carlo simulation, and all r...
Wind tunnel investigation for determination of subsonic and transonic aerodynamic characteristics of...
A wind tunnel study to determine the supersonic aerodynamic characteristics of a 0.01925-scale model...
Flight qualifications for parachutes were tested on full-scale simulated Viking spacecraft at entry ...
Force tests of a model of a proposed six-engine hull-type seaplane were performed in the Langley 8-f...
Tests of the Viking 16.15-meter nominal-diameter disk-gap-band parachute were conducted at Mach numb...
Results are presented for wind tunnel tests of a one to twelve scale model of the M2-F2 lifting body...
Transonic wind tunnel tests for aerodynamic characteristics of wing-body configuration