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Joined-Wing Wind-Tunnel Test for Longitudinal Control via Aftwing Twist
September 01, 2010
- Hollow Cathode Plume Velocity: Measurements and Modeling
- GPS constellation buildup plan
- Assessment of Rarefied Hypersonic Aerodynamics Modeling and Windtunnel Data
- Simulation of Pyrolysis Gas Within a Thermal Protection System
- Progress In NEXT Ion Optics Modeling
- A Low Diffusion Particle Method for Simulating Compressible Inviscid Flows
- Assessment of Gas-Surface Interaction Models in DSMC Analysis of Rarefied Hypersonic Flow
- Shuttle performance enhancement using an uprated OMS engine
- The T6 Hollow Cathode: Measurements and Modeling
- Effect of aluminum concentration in propellant on performance of rocket motors
- Uprated OMS engine status and future applications
- Comparison of Detailed Electron Fluid Model Formulations for Non-equilibrium Plasma Simulations
- Development in low cost nozzles
- Why Space Research and Space Exploration?: NASA Ames Research Center Contributions to NASA's 50 Years
- Hall thruster far field plume modeling and comparison to Express flight data
- A summary of spacecraft charging results
- Computation of Hypersonic Nonequilibrium Flows using the Direct Simulation Monte Carlo Method
- Extension of a Multiscale Particle Scheme to Near-Equilibrium Viscous Flows
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Complementary use of optical sensors and accelerometers in measuringtest pad stability.
June 01, 1966