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Flugtriebwerk
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Wing-Nacelle-Propeller Tests - Comparative Tests of Liquid-Cooled and Air-Cooled Engine Nacelles
Flight Tests of Exhaust Gas Jet Propulsion, Special Report
Wind-tunnel Tests of Four Curtiss Propellers Embodying Different Blade Sections
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
Static-Thrust Tests of Six Rotor-Blade Designs on a Helicopter in the Langley Full-Scale Tunnel
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
Natural icing of an axial-flow turbojet engine in flight for a single icing condition
Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine
Preliminary results of natural icing of an axial-flow turbojet engine
De-icing effectiveness of external electric heaters for propeller blades
Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine
Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine
Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine
Heat requirements for ice prevention on gas-heated propellers
Theoretical Investigations on the Efficiency and the Conditions for the Realization of Jet Engines
Icing-protection requirements for reciprocating-engine induction systems
NACA Conference on Some Problems of Aircraft Operation: A Compilation of the Papers Presented
Altitude Performance of J35-A-17 Turbojet Engine in an Altitude Chamber
Altitude Performance and Operational Characteristics of YJ71-A-7 Turbojet Engine
Aspects of Internal-Flow-System Design for Helicopter Propulsive Units
Over-All Performance of J65-B3 Turbojet Engine for Reynolds Number Indices from 0.8 to 0.2
Turbojet Lift Engine Design for VTOL Transports
VIII. Noise Considerations for Future Manned Aircraft
IV. Air-Breathing Propulsion Systems for Supersonic Aircraft
Apollo 7 Mission Report Communications System Performance
QCSEE task 2: Engine and installation preliminary design
Quiet Clean Short-Haul Experimental Engine (QCSEE). Preliminary analyses and design report, volume 2