Technical Report, Volume 3H.M. Stationery Office, 1946 - Aeronautics Includes its Reports, which are also issued separately. |
Contents
Introduction | 1546 |
Conclusions | 1557 |
Tests of a Centaurus Nacelle Installation with N A C A Cowl and Rear Swept Exhaust System | 1566 |
Copyright | |
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aerofoil air flow aircraft angle antisymmetrical approximately axis baffle constant calculated cent CHAMBER INLET MACH coefficient combustion chamber COMBUSTION CHAMBER INLET components compression compressor cooling cosh cowl entry curves cycle cylinder deadrise deflexion diffuser distribution drag dural effect efficiency elevator engine equation EQUIVALENT AIRSPEED exhaust factor Flight Mach Number flutter force frequency ft./sec fuel functions fuselage gas turbine gill exit GILL POSITION gills open given heat exchanger heat flow increase intercooling isentropic load longerons loss m₁ mass flow maximum measured method MINISTRY OF SUPPLY obtained oscillograph outlet output panel parameters pickup plane plotted pressure ratio propeller propulsive ramjet rivets roots rudder shear stress shown in Fig sideslip specific impulse stability stringers T₁ Table tailplane thrust torsional total head trim tunnel turbine values variation velocity vibration wing Young's modulus zero