SMALL ELECTRICALLY POWERED CONTRA-ROTATING TURBO FAN ENGINES FOR HIGH-SPEED AIRCRAFT APPLICATION
FLOW FIELD AND POWER BALANCE OF A DISTRIBUTED AFT-FUSELAGE BOUNDARY LAYER INGESTING AIRCRAFT
ANALYSIS OF IFCPT SDUCT USING OPENFOAM FOR THE 4TH AIAA PAW CONFERENCE
SUMMARY OF THE 4TH PROPULSION AERODYNAMICS WORKSHOP: S-DUCT RESULTS
INFLUENCE OF THE EXTERNAL FLOW CONDITIONS TO THE JET-VECTORING PERFORMANCES OF A SVC NOZZLE
PERFORMANCE ANALYSES OF FLUIDIC THRUST VECTOR CONTROL SYSTEM USING DUAL THROAT NOZZLE
THE IMPACT OF INLET BOUNDARY LAYER THICKNESS ON THE UNSTEADY AERODYNAMICS OF S-DUCT INTAKES
EXPERIMENT ON AIR INTAKE PERFORMANCE OF EJECTOR-JET USING WAX-BASED FUEL HYBRID ROCKET
BCFD, KESTREL ANALYSIS FOR THE 4TH AIAA PROPULSION AERODYNAMICS WORKSHOP: NOZZLE RESULTS
AN EXPERIMENTAL INVESTIGATION OF TURBO-RAMJET ENGINE INTAKE AT MACH 4
FUN3D, USM3D ANALYSIS OF THE PROPULSION AERODYNAMIC WORKSHOP 2018 S-DUCT TEST CASE
BCFD ANALYSIS FOR THE 4TH AIAA PROPULSION AERODYNAMICS WORKSHOP: SPECIAL TOPIC RESULTS
DEVELOPMENT OF A DUCTED PROPULSOR FOR BLI ELECTRIC REGIONAL AIRCRAFT PART II: AEROACOUSTIC ANALYSIS
A CFD INVESTIGATION OF A DIVERTERLESS SUPERSONIC INLET OF ELLIPSOIDAL ENTRANCE SHAPE
Supersonic Wake-Jet Interaction on a Rocket Afterbody with Dual-Bell Nozzles
Experimental study on the hazards of high-pressure hydrogen jet diffusion flames
Novel chevron nozzle concepts for jet noise reduction
Experimental study of flow behaviour and thermal loads in dual bell nozzles
Optimization for improved propulsive efficiency and increased bollard pull
Baureihe 2000. Kompakte Motoren bis 2000 kW
Präzisionsmeßtechnik im Fahrzeug. Einrichtung für den Serienabgleich
Laserüberwachung. Integrierte Profilprüfung von Kleberaupen in der Automobilindustrie
Dauerschwingfestigkeit : Schlußbericht zum Vorhaben
Two parallel plane jets: comparison of the performance of three turbulence models