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Kühlsystem
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Wind Tunnel Investigation of Rear Underslung Fuselage Ducts
Use of water injection to decrease gasoline consumption in an aircraft engine cruising at high power
Transpiration and Film Cooling of Liquid Rocket Nozzles
The effect of valve clearance on knock-limited performance and engine cooling
The effect of oil consumption and piston cooling on knock-limited aircraft-engine performance
The effect of cooling-air blowers on thrust power
The Edison Infrared Space Observatory and the Study of Extra-Solar Planetary Meterial
The Development of an Airborne Information Management System for Flight Test
Tests of Several Model Nacelle-propeller Arrangements in Front of a Wing
Supercooling of thermoelectric device using a current pulse
Summary of observed results when chilling the M-1 fuel turbopump to liquid hydrogen temperature