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Far-field calculations for turbofan noise

AIAA Journal, 2001
The development of variable-order mapped infinite wave envelope elements for finite element modeling of acoustic radiation from turbofan nacelles is reviewed. These elements can be used outside of the near field as a nonreflecting boundary condition and as a finite-dimensional discretization of the infinite exterior domain for calculation of far-field ...
Indranil Danda Roy, Walter Eversman
openaire   +1 more source

Smart Acoustic Lining for UHBR Technologies Engine Part 2: Acoustic Treatment at the Intake of a Scaled Turbofan Nacelle

Advanced Courses
The new generation of Ultra-High-By-Pass-Ratio (UHBR) turbofan engine while considerably reducing fuel consumption, threatens higher noise levels at low frequencies because of its larger diameter, lower number of blades and rotational speed.
E. de Bono   +7 more
semanticscholar   +1 more source

Affordable Smaller Turbofans

Volume 1: Turbo Expo 2005, 2005
Smaller smarter un-manned air vehicles (UAV’s) and missiles are being proposed and developed to function in a variety of roles previously performed by larger manned aircraft and limited range missiles. The endurance and stealth demanded of such advanced vehicles requires small turbofan engines possessing relatively higher power density combined with ...
openaire   +1 more source

Water-Augmented Turbofan Engine

Journal of Hydronautics, 1968
This paper describes a novel lightweight propulsion scheme for use in high-speed ships in which large amounts of water are injected into the fan discharge duct of an aircraft- type turbofan engine. Theoretical design and off-design performance for this water-augmented turbofan engine show that dry thrust theoretically can be augmented 380% at 25 knots ...
W. RICHARD DAVISON, THOMAS J. SADOWSKI
openaire   +1 more source

Uncertainty Analysis of Turbofan and Turboprop Architectures for Hybrid Electric Propulsion in NASA EPFD Vehicles

AIAA AVIATION FORUM AND ASCEND 2024
Hybrid Electric Propulsion (HEP) has garnered significant attention as part of the initiative to decarbonize the aviation industry by 2050. However, the ongoing development of the electrical components poses technological challenges, making the ...
Tavish Pattanayak   +5 more
semanticscholar   +1 more source

An Adaptive Dynamic Programming Scheme for Nonlinear Optimal Control With Unknown Dynamics and Its Application to Turbofan Engines

IEEE Transactions on Industrial Informatics, 2021
In this article, a novel adaptive dynamic programming (ADP) approach is proposed for the optimal control problem of nonlinear continuous control systems with unknown dynamics.
Tao Sun, Ximing Sun
semanticscholar   +1 more source

Multiobjective Optimization for Turbofan Engine Using Gradient-Free Method

IEEE Transactions on Systems, Man, and Cybernetics: Systems
Turbofan engine performance optimization is usually formulated as a single objective, closed-form optimization problem by employing a prior mechanism model with an additive, user-preference weight. However, in practical scenarios, the conventional single
Ran Chen   +3 more
semanticscholar   +1 more source

A Range of Turbofans

Aircraft Engineering and Aerospace Technology, 1989
PROGRESS in the development of turbofan engines for civil and military applications has enabled requirements from around 5,000lb to over 70,000lb thrust to be satisfied or anticipated, with prospects for this range to be extended. The three major powerplant manufacturers (Rolls‐Royce, General Electric and Pratt & Whitney) are engaged in fiercely ...
openaire   +1 more source

More Electric Small Turbofan

SAE Technical Paper Series, 2004
<div class="htmlview paragraph">The highly competitive aerospace industry demands the continuous improvement of aircraft propulsion engines and timely response to new and changing requirements for them. Turbofan engines are a relatively mature and sophisticated technology.
J. H. Brand   +3 more
openaire   +1 more source

Thermodynamic Analysis of Turbofan Engine

Volume 1: Turbo Expo 2005, 2005
The present work deals with a detailed parametric thermodynamic analysis of all the possible configurations of turbofan engine (two and three spool with or without mixer and/ afterburner) employing transpiration cooling technique for turbine blade cooling.
R. Yadav   +2 more
openaire   +1 more source

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