[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Mushtaq et al., 2023 - Google Patents

The role of endwall shape optimization in the design of supersonic turbines for rotating detonation engines

Mushtaq et al., 2023

View PDF
Document ID
11577617227299630232
Author
Mushtaq N
Persico G
Gaetani P
Publication year
Publication venue
Journal of Turbomachinery

External Links

Snippet

Rotating detonation engines (RDEs) are characterized by a thermodynamic cycle with an efficiency gain up to 15% at medium pressure ratios with respect to systems based on the conventional Joule–Bryton cycle. Multiple turbine designs can be considered, and this …
Continue reading at re.public.polimi.it (PDF) (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5086Mechanical design, e.g. parametric or variational design
    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • Y02T50/671Measures to reduce the propulsor weight
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING ENGINES OR PUMPS
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or anti-vibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction

Similar Documents

Publication Publication Date Title
Horlock et al. A review of some early design practice using computational fluid dynamics and a current perspective
John et al. Novel compressor blade shaping through a free-form method
Dow et al. The implications of tolerance optimization on compressor blade design
Kamenik et al. Robust turbine blade optimization in the face of real geometric variations
Ngetich et al. A three-dimensional conjugate approach for analyzing a double-walled effusion-cooled turbine blade
Germain et al. Improving efficiency of a high work turbine using nonaxisymmetric endwalls—Part I: endwall design and performance
Hergt et al. Advanced nonaxisymmetric endwall contouring for axial compressors by generating an aerodynamic separator—Part II: Experimental and numerical cascade investigation
Persico et al. Aerodynamics of centrifugal turbine cascades
Griffin et al. Simulations of the unsteady flow through the Fastrac supersonic turbine
Shahpar et al. Aerodynamic optimization of high-pressure turbines for lean-burn combustion system
Xu et al. Centrifugal compressor performance improvements through impeller splitter location
Nagel et al. Experimentally verified numerical optimization of a three-dimensional parametrized turbine vane with nonaxisymmetric end walls
Mushtaq et al. The role of endwall shape optimization in the design of supersonic turbines for rotating detonation engines
Cui et al. Low order modeling for fan and outlet guide vanes in aero-engines
Dorney et al. Effects of tip clearance on hot streak migration in a high-subsonic single-stage turbine
Munoz Lopez et al. The new chapter of transonic compressor cascade design at the DLR
Pazireh et al. A new loss generation body force model for fan/compressor blade rows: application to uniform and non-uniform inflow in rotor 67
Hottois et al. Comparing gradient-free and gradient-based multi-objective optimization methodologies on the VKI-LS89 turbine vane test case
Kluxen et al. Loss mechanisms of interplatform steps in a 1.5-stage axial flow turbine
Grasa et al. Design, multi-point optimization, and analysis of diffusive stator vanes to enable turbine integration into rotating detonation engines
Walker et al. Experimental and computational study of hybrid diffusers for gas turbine combustors
Vikhorev et al. Detailed experimental study of the flow in a turbine rear structure at engine-realistic flow conditions
Grimshaw et al. Loss in axial compressor bleed systems
Zhou et al. A shock loss reduction method using a concave suction side profile for a zero inlet swirl turbine rotor
Teia New supersonic loss model for the preliminary design of transonic turbine blades and the influence of pitch