Add to ORKGThe interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...
Statistical analysis of influencial aspects of wind profile disturbances design and dynamic response...
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Space vehicle flight control modes for basic wind profiles - reduction of aerodynamic loads for wind...
The results of a six degree of freedom (6-DOF) nonlinear Monte Carlo dispersion analysis for the lat...
Wind tunnel study of levels and spectra of pressure fluctuations acting on leeward side of straight ...
Experimental static aerodynamic data for Apollo, Saturn 5 launch vehicle configuration
Pressure distribution data have been obtained in flight at four span stations on the wing panel of t...
A 35 km grid limited area mesoscale model was initialized with high density SESAME radiosonde data a...
The effects of environmental perturbations on the attitude of a slow tumbling earth-oriented satelli...
This report discusses the development and underlying mathematics of a rigid-body computer model of a...
A recently developed storm electrification model (SEM) is used to investigate the operating environm...
A linear aircraft model for a rigid aircraft of constant mass flying over a flat, nonrotating earth ...
A generic, yet comprehensive mathematical model and computer simulation of the HLA flight dynamics o...
An experimental investigation is reported on slanted base ogive cylinders at zero incidence. The Mac...
The interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...
Statistical analysis of influencial aspects of wind profile disturbances design and dynamic response...
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...
Space vehicle flight control modes for basic wind profiles - reduction of aerodynamic loads for wind...
The results of a six degree of freedom (6-DOF) nonlinear Monte Carlo dispersion analysis for the lat...
Wind tunnel study of levels and spectra of pressure fluctuations acting on leeward side of straight ...
Experimental static aerodynamic data for Apollo, Saturn 5 launch vehicle configuration
Pressure distribution data have been obtained in flight at four span stations on the wing panel of t...
A 35 km grid limited area mesoscale model was initialized with high density SESAME radiosonde data a...
The effects of environmental perturbations on the attitude of a slow tumbling earth-oriented satelli...
This report discusses the development and underlying mathematics of a rigid-body computer model of a...
A recently developed storm electrification model (SEM) is used to investigate the operating environm...
A linear aircraft model for a rigid aircraft of constant mass flying over a flat, nonrotating earth ...
A generic, yet comprehensive mathematical model and computer simulation of the HLA flight dynamics o...
An experimental investigation is reported on slanted base ogive cylinders at zero incidence. The Mac...
The interaction of a two dimensional sonic jet injected transversely into a confined main flow was s...
Statistical analysis of influencial aspects of wind profile disturbances design and dynamic response...
Propulsion system requirements to support Low Earth Orbit (LEO) manned space station development and...