A survey of methods for turbojet thrust measurement applicable to flight installations
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Fleming, William A↗
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Results for “installations”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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The Effect of Inlet Installation on the Zero-lift Drag of a 60 Degree Delta-wing--body Configuration from Flight Tests at Mach Numbers from 0.8 to 1.86
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Merlet, Charles F↗
Effects of Rocket-armament Exhaust Gas on the Performance of a Supersonic-inlet J34-turbojet-engine Installation at Mach 2.0
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Beheim, Milton, A↗
Model Ditching Investigation of a Jet Transport Airplane with Various Engine Installations
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Thomson, William C↗
Static-pressure error calibrations for nose-boom airspeed installations of 17 airplanes
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Larson, Terry J↗
Effects of Free-stream Reynolds Number, Engine Installation, and Model Scale on Stability Characteristics of a Translating-spike Inlet at Mach 2.0
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Musial, Norman T↗
Flight Investigation of the Aerodynamic Forces on a Wing-mounted External-store Installation on the Douglas D-558-II Research Airplane
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Johnson, Clinton T↗
Performance of Multiple Jet-exit Installations
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Swihart, John M↗
Investigation at transonic speeds of a fixed divergent ejector installed in a single-engine fighter model
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Swihart, John M↗
Altitude-Wind-Tunnel Tests of Power-Plant Installation in Jet-Propelled Fighter
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AIRPLANES-BELL P-59A (WIND TUNNEL TESTS-AERL - TUR↗
Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel
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WING PANELS - GRUMMAN F4F-3↗
An Investigation of the Mutual Interference Effects of a Tail-surface : Stern Propeller Installation on a Model Simulating the Douglas XB-42 Empennage
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TAIL SURFACES - DOUGLAS B-42 - WIND TUNNEL TESTS (↗
Flight Investigation of Boundary-layer Transition and Profile Drag of an Experimental Low-drag Wing Installed on a Fighter-type Airplane
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DRAG, PROFILE↗
Full-scale-tunnel Investigation of a Multiengine Pusher-propeller Installation
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AIRFOILS - NACA 16-SERIES - PROPELLER↗
A study of the effect of aftercooling on the power and the weight of a 2000-horsepower air-cooled engine installation
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ENGINES-HORSEPOWER↗
Design, Selection, and Installation of Aircraft Heat Exchangers
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HEAT TRANSMISSION-ENGINES↗
Cooling Characteristics of a Pratt and Whitney R-2800 Engine Installed in an NACA Short-nose High-inlet-velocity Cowling
An investigation was made of the cooling characteristics of a P and W R-2800 engine with NACA short-nose high inlet-velocity cowling. The internal aerodynamics of the cowling were studied for ranges of propeller-advance ratio and inlet-velocity ratio obtained by deflection of cowling flaps. Tests included variations of engine power, fuel/air ratio and cooling-air pressure drop. Engine cooling data are presented in the form of cooling correlation curves, and an example for calculation of cooling requirements in flight is included.
HIGH-INLET-VELOCITY (SHORT-NOSE)↗
An Investigation of Cowl-flap and Cowl-outlet Designs for the Boeing B-29 Power-plant Installation
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ENGINE NACELLES-BOEING B-29↗