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Flugtriebwerk
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Wing-Nacelle-Propeller Tests - Comparative Tests of Liquid-Cooled and Air-Cooled Engine Nacelles
Drag and Propulsive Characteristics of Air-Cooled Engine-Nacelle Installations for Large Airplanes
Flight Tests of Exhaust Gas Jet Propulsion, Special Report
Performance Characteristics of an Aircraft Engine with Exhaust Turbine Supercharger
Wind-tunnel Tests of Four Curtiss Propellers Embodying Different Blade Sections
Construction of Finned Aluminum Muffs for Aircraft-Engine Cylinder Barrels
NACA Investigation of a Jet-Propulsion System Applicable to Flight
Analysis of the High-Altitude Cooling of the Ranger SGV-770 D-4 Engine in the Bell XP-77 Airplane
Recommended Test Procedure for Aircraft Engine Turbosupercharger Power Plants
Method of Mounting Cylinder Blocks of In-Line Engines on Cue Crankcases
Use of Water Injection to Decrease Gasoline Consumption in an Aircraft Engine Cruising at High Power
Static-Thrust Tests of Six Rotor-Blade Designs on a Helicopter in the Langley Full-Scale Tunnel
Determination of Air-Consumption Parameters for Two Radial Aircraft Engines
Requirements for Certification of Model C54E-DC airplane
BMW High Altitude Aircraft Engine Test Plant at Oberwiesenfeld (Near Munchen) Germany
Strain-Gage Study of Internally Cooled Exhaust Valves Having Various Throat Designs
Investigation of a Thermal Ice-Prevention System for a Twin-Engine Transport Airplane
Hydraulic Characteristics of the NACA Injection Impeller
Further Development of Heat-Resistant Materials for Aircraft Engines
Preliminary Study of a Propeller Powered by Gas Jets Issuing from the Blade Tips
A method for estimating heat requirements for ice prevention gas heated hollow propeller blades
A flight investigation of the thermal performance of air heated propeller
Performance Possibilities of the Turbojet System as a Power Plant for Supersonic Airplanes
Wind-tunnel investigation of icing of an engine cooling-fan installation
Possibilities of Reducing the Length of Axial Superchargers for Aircraft Motors
Performance of a Double-Row Radial Aircraft Engine with Three Methods of Safety-Fuel Injection
Effect of Exhaust Pressure on the Performance of a 12-Cylinder Liquid- Cooled Engine