Results 81 to 90 of about 3,568 (253)
Multi-variable control of the GE T700 engine using the LQG/LTR design methodology [PDF]
, 1986 "Proceeding American Control Conference, Seattle, WA, June 1986."Bibliography: p. 8.Research supported by General Electric Company. NASA Ames and Langley Research Centers grant NASA NAG2-297William H. Pfeil, Michael Athans, H.
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Feasibility of water injection into the turbine coolant to permit gas turbine contingency power for helicopter application [PDF]
A system which would allow a substantially increased output from a turboshaft engine for brief periods in emergency situations with little or no loss of turbine stress rupture life is proposed and studied analytically.
Vanfossen, G. J.
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The convertible engine: A dual-mode propulsion system [PDF]
A variable inlet guide vane (VIGV) convertible engine that could be used to power future high-speed rotorcraft was tested on an outdoor stand. The engine ran stably and smoothly in the turbofan, turboshaft, and dual (combined fan and shaft) power modes ...
Mcardle, Jack G.
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A Practical Approach to Modeling and Performance Analysis of a Turboshaft Engine Using Matlab
Applied SciencesThis article presents a detailed approach to constructing a numerical model of a free power turbine engine specifically designed for performance analysis in the Matlab R2024b environment.
Robert Jakubowski, Piotr Jakliński
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Study of an advanced General Aviation Turbine Engine (GATE) [PDF]
The best technology program for a small, economically viable gas turbine engine applicable to the general aviation helicopter and aircraft market for 1985-1990 was studied.
Curry, C. E. +7 more
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Summary of emissions reduction technology programs [PDF]
, 1977 The NASA emissions reduction contract programs for EPA aircraft engine classes P2 (turboshaft engines), T1 (jet engines with thrust under 8000 lb), T4 (JT8D) engines), and T2 (jet engines with thrust over 8000 lb) are discussed.
Niedzwiecki, R. W.
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Rotorcraft convertible engine study [PDF]
The objective of the Rotorcraft Convertible Engine Study was to define future research and technology effort required for commercial development by 1988 of convertible fan/shaft gas turbine engines for unconventional rotorcraft transports. Two rotorcraft
Earle, R. V., Gill, J. C., Mar, H. M.
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A generalized computer code for developing dynamic gas turbine engine models (DIGTEM) [PDF]
This paper describes DIGTEM (digital turbofan engine model), a computer program that simulates two spool, two stream (turbofan) engines. DIGTEM was developed to support the development of a real time multiprocessor based engine simulator being designed ...
Daniele, C. J.
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Design and Analysis of Gear System for Turboshaft Aero Engine Reduction Gearbox [PDF]
, 2016 Ritu Jacob Boby, E. Raj Kumar
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