المؤلفون: Cunningham, Cameron C.

المساهمون: WRIGHT LAB WRIGHT-PATTERSON AFB OH

المصدر: DTIC AND NTIS

مصطلحات موضوعية: Electrical and Electronic Equipment, Hydraulic and Pneumatic Equipment, VIBRATION, PRESSURE TRANSDUCERS, STAINLESS STEEL, OPERATIONAL EFFECTIVENESS, GAS TURBINES, TABLES(DATA), FREQUENCY RESPONSE, PNEUMATIC ACTUATORS, SHAKING, AXIAL FLOW COMPRESSORS, PE61102F, WUWL2307S127

وصف الملف: text/html

Relation: http://www.dtic.mil/docs/citations/ADA321086

الاتاحة: http://www.dtic.mil/docs/citations/ADA321086
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA321086

المؤلفون: Boyer, Keith

المساهمون: WRIGHT RESEARCH AND DEVELOPMENT CENTER WRIGHT-PATTERSON AFB OH AERO PROPULSION AND POWER LAB

المصدر: DTIC AND NTIS

مصطلحات موضوعية: Jet and Gas Turbine Engines, AIRCRAFT ENGINES, GAS TURBINES, STALLING, CENTRIFUGAL COMPRESSORS, COMPRESSION, CONTROL, AVIATION SAFETY, STALL CONTROL, HELMHOLTZ FREQUENCY, PE61102F, WUWL2307S127

وصف الملف: text/html

Relation: http://www.dtic.mil/docs/citations/ADA291275

الاتاحة: http://www.dtic.mil/docs/citations/ADA291275
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA291275

المؤلفون: Puterbaugh, Steven L.

المساهمون: WRIGHT LAB WRIGHT-PATTERSON AFB OH

المصدر: DTIC AND NTIS

مصطلحات موضوعية: Computer Programming and Software, Hydraulic and Pneumatic Equipment, Mechanics, COMPUTER PROGRAMS, POSITION(LOCATION), FORTRAN, SHOCK, PATTERNS, CONTOURS, PRESSURE DISTRIBUTION, PLOTTING, WAVES, TRANSONIC FLOW, COMPRESSOR ROTORS, INPUT, STATIC PRESSURE, WUWL2307S127, PE61102F, EXPERIMENTAL DATA, KPLOT COMPUTER PROGRAM, KULITES

وصف الملف: text/html

Relation: http://www.dtic.mil/docs/citations/ADA242760

الاتاحة: http://www.dtic.mil/docs/citations/ADA242760
http://oai.dtic.mil/oai/oai?&verb=getRecord&metadataPrefix=html&identifier=ADA242760

المؤلفون: WRIGHT LAB WRIGHT-PATTERSON AFB OH, Richardson, Scott M.

المصدر: DTIC AND NTIS

مصطلحات الفهرس: Fluid Mechanics, COMPUTATIONAL FLUID DYNAMICS, UNSTEADY FLOW, MATHEMATICAL MODELS, ALGORITHMS, STRESS ANALYSIS, GRIDS, BOUNDARY LAYER, TURBULENCE, TURBULENT FLOW, EDDIES(FLUID MECHANICS), VORTEX SHEDDING, FLOW FIELDS, INTERPOLATION, MACH NUMBER, DRAG, LIFT, NAVIER STOKES EQUATIONS, INVISCID FLOW, VISCOUS FLOW, VISCOSITY, PRESSURE DISTRIBUTION, REYNOLDS NUMBER, SKIN FRICTION, RUNGE KUTTA METHOD, TRANSONIC FLOW, TURBOMACHINERY, COMPRESSOR ROTORS, THREE DIMENSIONAL FLOW, CASCADES(FLUID DYNAMICS), ROTOR BLADES(TURBOMACHINERY), TURBINE STATORS, SMOOTHING(MATHEMATICS)., PE61102F, WUWL2307S127, Text

URL: https://apps.dtic.mil/docs/citations/ADA310237

المؤلفون: WRIGHT LAB WRIGHT-PATTERSON AFB OH, Cunningham, Cameron C.

المصدر: DTIC AND NTIS

مصطلحات الفهرس: Electrical and Electronic Equipment, Hydraulic and Pneumatic Equipment, VIBRATION, PRESSURE TRANSDUCERS, STAINLESS STEEL, OPERATIONAL EFFECTIVENESS, GAS TURBINES, TABLES(DATA), FREQUENCY RESPONSE, PNEUMATIC ACTUATORS, SHAKING, AXIAL FLOW COMPRESSORS., PE61102F, WUWL2307S127, Text

URL: https://apps.dtic.mil/docs/citations/ADA321086

المؤلفون: WRIGHT RESEARCH AND DEVELOPMENT CENTER WRIGHT-PATTERSON AFB OH AERO PROPULSION AND POWER LAB, Boyer, Keith

المصدر: DTIC AND NTIS

مصطلحات الفهرس: Jet and Gas Turbine Engines, AIRCRAFT ENGINES, GAS TURBINES, STALLING, CENTRIFUGAL COMPRESSORS, COMPRESSION, CONTROL, AVIATION SAFETY., STALL CONTROL, HELMHOLTZ FREQUENCY, PE61102F, WUWL2307S127, Text

URL: https://apps.dtic.mil/docs/citations/ADA291275

المؤلفون: WRIGHT LAB WRIGHT-PATTERSON AFB OH, Puterbaugh, S. L.

المصدر: DTIC AND NTIS

مصطلحات الفهرس: Computer Programming and Software, USER MANUALS, LIBRARIES, GRAPHICS, MICROCOMPUTERS, OUTPUT, FORTRAN, COMPUTER GRAPHICS, PE61102F, WUWL2307S127, FORTRAN-77 PROGRAMMING LANGUAGE, SUBROUTINES, CGRAPH SUBROUTINES., Text

URL: https://apps.dtic.mil/docs/citations/ADA242870

المؤلفون: WRIGHT LAB WRIGHT-PATTERSON AFB OH, Puterbaugh, Steven L.

المصدر: DTIC AND NTIS

مصطلحات الفهرس: Computer Programming and Software, Hydraulic and Pneumatic Equipment, Mechanics, COMPUTER PROGRAMS, POSITION(LOCATION), FORTRAN, SHOCK, PATTERNS, CONTOURS, PRESSURE DISTRIBUTION, PLOTTING, WAVES, TRANSONIC FLOW, COMPRESSOR ROTORS, INPUT, STATIC PRESSURE, WUWL2307S127, PE61102F, EXPERIMENTAL DATA, KPLOT COMPUTER PROGRAM, KULITES., Text

URL: https://apps.dtic.mil/docs/citations/ADA242760