Inlet, engine, airframe controls integration development for supercruising aircraftIn connection with a consideration of advanced military aircraft systems, attention is given to research for improving the technology of the design of supersonic cruise aircraft. Syberg et al. (1981) have shown that an analytic design method is now available to accurately predict the flow characteristics of axisymmetric supersonic inlets, including off-design angle of attack operation. On the basis of information regarding the inlet flow characteristics, the control system designer can begin the inlet design and development, before wind tunnel testing has begun. The present investigation is concerned with details and status of inlet control technology. A detailed representation of a supersonic propulsion system is developed. This development demonstrates the feasibility of the selected hybrid computational concept.
Document ID
19830054624
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Houchard, J. H. (Boeing Military Airplane Development Seattle, WA, United States)
Carlin, C. M. (Boeing Military Airplane Development Seattle, WA, United States)
Tjonneland, E. (Boeing Military Airplane Co. Seattle, WA, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: International Symposium on Air Breathing Engines