A unified analytical approach for the acoustic conceptual design of fans of modern aero-engines
A unified analytical approach for the acoustic conceptual design of fans of modern aero-engines
A unique coannular plug nozzle jet noise prediction procedure
AUTOIGNITION DELAY TIMES MEASUREMENTS OF LINEAR UNSATURATED JET FUEL COMPOUNDS INSIDE A SHOCK TUBE
AXIAL ROTOR DESIGN UNDER CLEAN AND DISTORTION CONDITIONS USING MEAN-LINE AND CFD METHODS
Benefits of blade sweep for advanced turboprops
Betrachtung des Verhaltens von Bürstendichtungen unter wechselnden Betriebsbedingungen
Betrachtung des Verhaltens von Bürstendichtungen unter wechselnden Betriebsbedingungen
"Buzz-saw" noise: Prediction of the rotor-alone pressure field
CAPTURING AERO-PROPULSIVE COUPLING EFFECTS WITH A BODY-FORCE PROPULSOR MODEL
Ceramic applications in turbine engines (CATE) program summary
CHARACTERIZATION OF A LASER DIAGNOSTIC SENSOR FOR GAS TURBINE COMBUSTER FLOWS
CHARACTERIZATION OF NON-REACTING SWIRLING FLOW IN A GAS TURBINE FUEL INJECTOR
Clean hydraulic systems. An approach to design and manufacture
CO2 SENSITIZED PROPANE OXIDATION AT 100 ATM IN A NOVEL JET STIRRED REACTOR
COMPUTATIONAL AND EXPERIMENTAL ASSESSMENT OF RIM SEALING FLOWS IN AXIAL TURBINE CHUTE RIM SEALS
COMPUTATIONAL INLET SWIRL DISTORTION INVESTIGATION OF A HIGH-SPEED COMPRESSOR
CONJUGATE HEAT TRANSFER STUDY OF INNOVATIVE PIN-FIN COOLING Configurations
DATA-DRIVEN COMBUSTION KINETIC MODELING CONCEPT OF ALTERNATIVE ALCOHOL-TO-JET (ATJ) FUEL
DEFINING A TESTBED FOR THE U.S. TURBINE INDUSTRY: THE NATIONAL EXPERIMENTAL TURBINE (NEXT)
Dehn-Schrumpf-Verband an einem hochtourig drehenden skalierten Flugtriebwerks-Rotor
DESCRIPTION AND APPLICATION OF A SOFTWARE TOOL FOR SIMULATION OF TOMOGRAPHIC PIV DATA
DESIGN, ANALYSIS, AND TESTING OF A LOW-COST, ADDITIVELY-MANUFACTURED, SINGLE-USE COMRESSOR
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
Design and life assessment of aeroengine components
DESIGN CONSIDERATIONS FOR EXTRA HIGH-PRESSURE RATIO (70) CIVIL AERO ENGINE LOW-EMISSION COMBUSTOR
DESIGN EXPLORATION FOR AN AXISYMMETRIC REAR BLI PROPULSOR
DESIGN OF A GEARED TURBOFAN MODULE FOR SMALL, UNMANNED AIRCRAFT APPLICATIONS