Active trim panel attachments for control of sound transmission through aircraft structures
Aerodynamic assessment of methods to simulate flight inflow characteristics during static testing
Aircraft drag reduction, the application of natural laminar flow to aero-engine nacelles
Aircraft engines join thrust for lower emission levels
A LOW ORDER MODELING APPROACH TO TRANSVERSE COMBUSTION INSTABILITY
Analyse und Vergleich fertigungstechnischer Prozessketten für Flugzeugtriebwerks-Rotoren
Analyse und Vergleich fertigungstechnischer Prozessketten für Flugzeugtriebwerks-Rotoren
APPLICATION OF DYNAMIC ZONE FLAMELET MODEL TO A GH2/GO2 ROCKET COMBUSTOR
Application of Navier-Stokes methods for engine/airframe integration
Auftragschweissen von Dichtstegen bei der Instandsetzung von Flugtriebwerken
A unique coannular plug nozzle jet noise prediction procedure
Benefits of blade sweep for advanced turboprops
BREAKUP CHARACTERISTICS AND FAR-FIELD TRAJECTORY OF LIQUID JETS IN SUBSONIC CROSSFLOW
BROADBAND, MID-INFRARED LASER-ABSORPTION MEASUREMENTS OF TEMPERATURE, CH4, AND C3H8 IN FLAMES
BURNING RATE CHARACTERIZATION OF AMMONIUM PERCHLORATE PELLETS CONTAINING CATALYTIC ADDITIVES
Ceramic applications in turbine engines (CATE) program summary
CHARACTERISTICS OF A PREMIXED REACTING JET-IN-CROSSFLOW AT ELEVATED PRESSURES
CHARACTERIZATION OF THE MELT LAYER OF AMMONIUM PERCHLORATE SINGLE
COMBUSTION BEHAVIOR OF AMMONIUM PERCHLORATE AT HIGH PRESSURES
COMBUSTION OF BORON, MAGNESIUM DIBORIDE PARTICLES IN LOW EQUIVALENCE RATIO METHANE FLAMES
COMBUSTOR DEVELOPMENT AND PERFORMANCE ANALYSIS FOR RECUPERATED MICROTURBINE APPLICATION
DESIGN AND CHARACTERIZATION OF THE DUAL INDEPENDENT SWIRL COMBUSTOR FACILITY (DISCO)
Design and life assessment of aeroengine components
DESIGN AND TEST OF A SHOCK TUBE FACILITY TO INVESTIGATE DROPLET AEROBREAKUP
DETERMINATION OF HEAT OF VAPORIZATION AND VAPOR PRESSURE BY MICRO-LITER FUEL DROPLET VAPORIZATION
DETERMINATION OF NITRIC OXIDE CONCENTRATIONS IN MIXTURES WITH NITROGEN TETROXIDE VIA IR SPECTROMETRY
DEVELOPMENT AND TESTING OF PULSE GUNS FOR COMBUSTION INSTABILITY TESTING