同源图形

TORNADO AIRCRAFT IN	TURBO UNION RB199 TU	EFFECT OF SWIRL AND
WILLIAMS INTERNATION	TOMAHAWK INLET/ENGIN	DUAL FAN CHARACTERIS
FAN-IN-WING CROSS SE	LIFT FAN INSTALLATIO	LIFT-FAN STREAM TUBE
JSF PROPULSION SYSTE	B52/JT9D REVERSER TE	C-141/TF33 INLET DIS
APU INSTALLED IN AIR	APU INLET DUCT SWIRL	DEFINITION OF SWIRL
PROJECTED VELOCITY V	BULK SWIRL GENERATED	PLENUM-STYLE INLET I
AN INLET DUCT WITH A	EXAMPLE OF TORNADO S	PHOTOGRAPH OF A TIGH
FUSELAGE-MOUNTED ENG	VELOCITY RATIO VERSU	COMPARISON OF GROUND
INFLUENCE OF WIND DI	VELOCITY DISTRIBUTIO	FORMATION OF A PAIRE
OFFSET SWIRL PAIR DE	FORMATION OF A PAIRE	PROJECTED VELOCITY V
PLENUM STYLE INLETS	TOTAL PRESSURE AND P	NACA SCOOP IN STATIC
PAIRED VORTEX SWIRL	CIRCUMFERENTIAL DIST	CROSS-FLOW SWIRL DIS
SWIRL GENERATED BY A	PROJECTED VELOCITY V	VELOCITY DIAGRAMS AT
EFFECT OF PURE BULK	TYPICAL ONE-PER-REV	SPECTRUM OF SWIRL DI
EXAMPLE VALUES OF SW	EXAMPLE VALUES OF SW	EXAMPLE VALUES OF SW
EXAMPLE VALUES OF SW	STABILITY MARGIN DEF	SENSOR LOCATIONS FOR
COBRA PROBE (REFEREN	MACH/FLOW ANGULARITY	EXAMPLE INLET MODEL
EXAMPLE OF CFD FOR I	APU TEST INSTALLATIO	TOTAL PRESSURE DISTO
SWIRL MEASURED IN AP	TYPICAL SERPENTINE-T	TYPICAL TOTAL PRESSU
TYPICAL CFD CALCULAT	TYPICAL CFD CALCULAT	TRADITIONAL TOTAL PR
SWIRL DESCRIPTORS AS	COMPUTED SWIRL PATTE	COMPUTED SWIRL PATTE
TOTAL PRESSURE DISTO	DIRECT-CONNECT TEST	BULK AND TWIN SWIRL
SWIRL GENERATORS THA	SWIRL GENERATOR THAT	COMPRESSOR MAP MODIF
PARALLEL COMPRESSOR	EFFECT OF PRESSURE D	IMPOSED CIRCUMFERENT
EFFECT OF PAIRED SWI	EFFECT OF IN-PHASE S	EFFECT OF OUT-PHASE
FIGHTER AND CRUISE M	FREE-JET TEST SCHEMA	TORNADO ENGINE INTAK
EFFECT OF ANGLE OF A	SECONDARY FLOWS IN I	MAXIMUM, MEAN AND MI
SECONDARY FLOWS IN I	FLOW ANGLES AND ISOB	MAXIMUM, MEAN AND MI
TOMAHAWK INLET/ENGIN	INLET VARIABILITY OB	EXHAUST TEMPERATURE
VORTEX SYSTEM 10MM A	COMPUTED VORTEX SYST	TWIN TWO-PER-REV SWI
AN IDEALIZED TWO-PER	SWIRL DIRECTIVITY SP	SWIRL PAIRS SPECTRUM
TWIN TWO-PER-REV SWI	EXAMPLE OF A TWIN TW	ILLUSTRATION OF SECT
CONFIGURATIONS TESTE	SWIRL REDUCTION: (A)	EXTENSION OF ANGLE O
EXTENSION OF MACH NU