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Flugtriebwerk
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NASA Meeting on Cryogenic Fuel Systems for Aircraft: Overview of Previous Workshops and Studies
Aqueous, Quick-Charging Battery Integration for Electric Flight Research (AQUIFER)
AQUIFER Review of AQUIFER Technology Feasibility June 15 -- 19, 2020
Optimization of a Parametric Lobe Mixer for Internally Mixed Nozzles
Effects of Spent Cooling and Swirler Angle on a 9-Point Swirl-Venturi Injector
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 2 of 2
Experimental Study of Turbine Fuel Thermal Stability in an Aircraft Fuel System Simulator
Propellants and combustion / American Institute of Aeronautics and Astronautics ; Volume 1 of 2
Application of automobile emission control technology to light piston aircraft engines
Study of the application of hydrogen fuel to long-range subsonic transport aircraft, volume 2
Emissions and new technology programs for conventional spark-ignition aircraft engines
Ceramic regenerator systems development program
Status of the NASA/General Electric experimental clean combustor program, phase 3
Energy consumption characteristics of transports using the prop-fan concept
Development of EPA aircraft piston engine emission standards
Advanced low emissions catalytic combustor program at Pratt and Whitney
Results and status of the NASA aircraft engine emission reduction technology programs
NUMERICAL STUDY ON COMBUSTION CHARACTERISTIC OF MICRON ALUMINUM PARTICLE
Upper atmosphere pollution measurements (GASP)
Analysis of the High-Altitude Cooling of the Ranger SGV-770 D-4 Engine in the Bell XP-77 Airplane
EFFECT OF FUEL TEMPERATURE ON EMISSIONS AND STRUCTURE OF A SWIRLSTABILIZED FLAME
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)