This content is not included in your SAE MOBILUS subscription, or you are not logged in.
DEVELOPMENT OF A CABIN PRESSURE CONTROL SYSTEM FOR TRANSPORT TYPE AIRCRAFT
ISSN: 0148-7191, e-ISSN: 2688-3627
Published January 01, 1956 by SAE International in United States
Annotation ability available
To provide maximum comfort for passengers, it is claimed that cabin pressures must be maintained within very-narrow limits. The various steps by which a system was developed to accomplish such control is discussed and illustrated by photographs and diagrams. The author believes that the final result of the research and development program is a system which will not only provide the necessary control, but will do so with a degree of reliability unknown in earlier systems, with a minimum of maintenance and extremely simple in operation. Two production systems are described in detail with a final explanation of how a transistorized pre-amplifier and magnetic amplifier is used.
|Technical Paper||PROSPECTS FOR DRAG PREDICTION USING COMPUTATIONAL FLUID DYNAMICS|
|Technical Paper||Computational Aerodynamics in Aircraft Design: Challenges and Opportunities for Euler/Navier-Stokes Methods|