Turboprop cargo aircraft systems study [PDF]
The effects of using advanced turboprop propulsion systems to reduce the fuel consumption and direct operating costs of cargo aircraft were studied, and the impact of these systems on aircraft noise and noise prints around a terminal area was determined.
Hewell, J. G., Jr. +5 more
core +1 more source
A computer program for calculating design and off-design performance for turbojet and turbofan engines [PDF]
, 1973 Program uses component performance maps to enable user to do analytical engine cycle calculations. Through scaling procedure, each of the component maps can be used to represent a family of maps.
Fishbach, L. H., Koenig, R. W.
core +1 more source
A remote augmentor lift system with a turbine bypass engine [PDF]
Two supersonic vertical takeoff or landing (VTOL) aircraft engine types, a conventional medium bypass ratio turbofan, and a turbine bypass turbojet were studied. The aircraft assumed was a clipped delta wing with canard configuration.
Fishbach, L. H., Franciscus, L. C.
core +1 more source
Patent Citations as Signals of Technical Interactions: The Case of a Turbofan Jet Engine
, 2023 Guillermo Ruiz Pava +2 more
openalex +1 more source
Computer-Aided Design of Structural Elements of Modern Turbofan Compressors
, 2017 Александр Евгеньевич Кишалов +1 more
openalex +1 more source
Holistic performance evaluation of a turbofan featuring pressure gain combustion for a short-range mission [PDF]
, 2023 Nicolai Neumann, Dieter Peitsch
openalex +1 more source
HYTESS 2: A Hypothetical Turbofan Engine Simplified Simulation with multivariable control and sensor analytical redundancy [PDF]
A hypothetical turbofan engine simplified simulation with a multivariable control and sensor failure detection, isolation, and accommodation logic (HYTESS II) is presented.
Merrill, W. C.
core +1 more source
Eulerian and Lagrangian Ice-Crystal Trajectory Simulations in a Generic Turbofan Compressor
, 2018 Ellen Norde +5 more
openalex +2 more sources
Effect of forward motion on engine noise [PDF]
Methods used to determine a procedure for correcting static engine data for the effects of forward motion are described. Data were analyzed from airplane flyover and static-engine tests with a JT8D-109 low-bypass-ratio turbofan engine installed on a DC-9-
Blankenship, G. L. +3 more
core +1 more source