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Fluidmechanik
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The Orbiting Geophysical Observatory Test and Support Program
The NASA Microgravity Fluid Physics Program: Research Plans for the ISS
The NASA Microgravity Fluid Physics Program: Knowledge for Use on Earth and Future Space Missions
The NASA Ames Aerothermodynamics Branch (Code TSA)
The NASA Ames 16-Inch Shock Tunnel Nozzle Simulations and Experimental Comparison
THE LANTHANUM, EUROPIUM, AND DYSPROSIUM CONTENTS OF TWO TEKTITES
The Lag Model, a Turbulence Model for Wall Bounded Flows Including Separation
The International Heat Pipe Experiment
The International Heat Pipe Experiment
The Influence of Computer Architecture on Performance and Scaling for Hypersonic Flow Simulations
The Importance of Thermostructural Testing Hypersonic Structures
The hydraulic characteristics of flow through miniature slot orifices
The hub wall boundary layer development and losses in an axial flow compressor rotor passage
The Formation and Properties of Liquid Sheets Suitable for Use in Rocket Engine Injectors
The Effects of Propellant Slosh Dynamics on the Solar Dynamics Observatory
The Effects of Propellant Slosh Dynamics on the Solar Dynamics Observatory
The Effect of Metallic TPS Panel Bowing on the Surface Heating of the X-33 Vehicle
The effect of inflow velocity profiles on the performance of supersonic ejector nozzles
The dynamic behavior of liquids in moving containers - Introduction
The Direction of Fluid Dynamics for Liquid Propulsion at NASA Marshall Space Flight Center
The Direction of Fluid Dynamics for Liquid Propulsion at NASA Marshall Space Flight Center
The Design of a High-Q, MACH-5 Nozzle for the Langley 8-Foot HTT
The Current Status of Unsteady CFD Approaches for Aerodynamic Flow Control
THE COMPARISON AND COMBINATION OF SATELLITE WITH OTHER DETERMINATIONS OF GEODETIC PARAMETERS
The calculation of the heat required for wing thermal ice prevention in specified icing conditions
The application of Riegels' rule and time-like damping to transonic flow calculations
The Aerospace Plane Design Challenge: Credible Computational Fluid Dynamics Results
The Active Thermal Architecture: Active Thermal Control for Small-Satellites
Thales Tactical Pulse Tube Cryocooler Testing Status
Tests on a sodium/Hastelloy X wing leading edge heat pipe for hypersonic vehicles
Tests of Cascades of Airfoils for Retarded Flow
Test results of prototype two-phase reservoirs for the CAPL flight experiment
Testing of the Crew Exploration Vehicle in NASA Langley's Unitary Plan Wind Tunnel
Testing Microgravity Flight Hardware Concepts on the NASA KC-135
Test Cases for NASA's Revolutionary Computational Aerosciences Technical Challenge
TESSERAL HARMONICS OF THE POTENTIAL OF THE EARTH AS DERIVED FROM SATELLITE MOTIONS
Tenth Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion, Part 1