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Fluidmechanik
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Transonic Unsteady Aerodynamics for Planar Wings with Trailing Edge Control Surfaces
The use of computer simulation in the evaluation of electric vehicle batteries
Systematische Optimierung des Thermomanagements eines batterieelektrischen Sportwagens
Systematische Optimierung des Thermomanagements eines batterieelektrischen Sportwagens
Statistical Analysis of Flight Vibration and Acoustic Data
Propulsion System Integration and Test Program (Steady State). Part IV. Inlet Drag Tests
Professional Papers Cleared for Possible Publication and/or Presentation
Numerische Analyse der Zweiphasenströmung und Kühlwirkung in nasslaufenden Elektromotoren
Nonlinear Lift and Pressure Distribution of Slender Conical Bodies with Strakes at Low Speeds
National Aerospace Plane (NASP): Development Issues for the Follow-on Vehicle
Micro-Scale Avionics Thermal Management
Micro- and Nano-Scale Electrically Driven Two-Phase Thermal Management
Micro- and Nano-Scale Electrically Driven Two-Phase Thermal Management
Investigation of Gaseous Nuclear Rocket Technology. Summary Technical Report
Integrated simulation and testing of electric vehicle batteries
Injector Service Study, APOLLO Service Propulsion System Final Report, 7 Apr. 1967 - 31 Jul. 1968
Initial Experiments to Investigate Condensation of Flowing Metal-Vapor/Heated-Gas Mixtures in a Duct
Hypersonic Aerodynamic Flow around Slender Cones at High Incidence, Part 1 B
GEOPHYSICAL RESEARCH WITH SATELLITES INJUNS I, II, AND III
Fundamentals of the Aerodynamics of Hypersonic Velocities
Flow Fields over Sharp Edged delta Wings with Attached Shocks
Experimental Investigation of Peripheral-Wall Injection Techniques in a Water Vortex Tube
Experimental Investigation of Nozzle/Plume Aerodynamics at Hypersonic Speeds
Experimental Investigation of Containment in Constant-Temperature Radial-Inflow Vortexes
Embedded Thermal Control for Spacecraft Subsystems Miniaturization
Effect of Incidence and Reynolds Number on Hypersonic Flow past a Circular Cone
Dynamic Stability of Space Vehicles. Volume 14 - Testing for Booster Propellant Sloshing Parameters
Dynamic Radioisotope Power Systems Development Status and Path to Flight
Development of Advanced Spacecraft Thermal Subsystems