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Title

AeroRocket simulation software for rockets and airplanes

Description

AeroRocket, source for AeroCFD, AeroDRAG, VisualCFD and other aerodynamics software.

Keywords

rocket, airplane, AeroCFD, aerocfd, aero cfd, Aero CFD, aerodynamics, VisualCFD, micro-cfd, AeroDRAG, John Cipolla, AeroIsp, Nozzle, CFD, drag, Cd, Cp, drag coefficient, solid rocket motor, thrust, chamber pressure, wind tunnel, star travel, StarTravel, supersonic, hypersonic, subsonic, aerodynamics, aerospike, airfoil, fin, wing

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Text Analysis

Cloud of Keywords from all content
High relevance
 

tunnel nozzle wind aerorocket visualcfd supersonic rocket flow pressure blow-down analysis shapes diameter validation plots cells shock subsonic ratio

Medium relevance
 

axisymmetric startravel number direction testing rockets velocity constant software variable waves exhaust cipolla model geometry john two-dimensional coefficient aerodynamics performs standard version aerocfd flight

Low relevance
 

variable waves exhaust cipolla model geometry john two-dimensional coefficient aerodynamics performs standard version aerocfd flight heliocentric angle axial orbital non-zero vertical library compressible impulse fabrication program sections center temperature astrodynamics analyses two-body typical airplanes generate determine burnout density amateur thickness drag addition latest | visualcfd designed simulation warpmetrics power drive fluid designs cfd | nozzle include overexpanded user

Very Low relevance
 
heliocentric angle axial orbital non-zero vertical library compressible impulse fabrication program sections center temperature astrodynamics analyses two-body typical airplanes generate determine burnout density amateur thickness drag addition latest | visualcfd designed simulation warpmetrics power drive fluid designs cfd | nozzle include overexpanded user measurement tool 100k ranging simple aerorocket customer line-contour miniature engineering models high expertise complex probe pitot-static displayed fields total measuring process measured x-30 htv-3x nasp verses fill-contour surface measurements curve static motor team aerodynamic aeropac supersonic prize airframe tools winning superior consulting contact biba carmack inside-diameter testing aerocfd multiple single easily rocketry derive sets factor blockage joins customer supersonic blow-down distribution performance vasimr magnetoplasma rocket perform nuclear propulsion 2013 top starting v-2 horizontally registered ballistic ability to trajectory missiles vertically launched planets stars propulsion x-30 plasma and vasimr nasp spaceshipone htv-3x validation analyses shock 1999-2013 | model books ducted propulsion reference | aerospike trademark links magnetic updated and warp levitation transfer hohmann starship vasimr copyright tube service wind software customer satellites spacecraft compared eternity quicktime view click movie segment seconds maintained comments knowing earth motion interplanetary sun spaceplane analysis | ss1 general | rocket sub-orbital flight-path | companies purpose pressure predicting dominate determining case selecting internal converging-diverging nozzles variation entirely supersonic combination are clearly diverging including shock area cross-sectional external aerodynamicist chief pattern ssme isentropic one-dimensional identified lines real-time displays slider values of properties shock-angle ability to ratio and color contours types selecting from cross-sectional shape defining geometry using method free-form tunnels fabricated aeroisp™ aerospike 2d-wing™ aerodrag aerocp™ aerofinsim™ hypercfd™ products aerowindtunnel™ banned november affordable providing product consulting resume mission aeroeuler™ startravel™ physics warp dynamics aerospace development services gliders computational hypersonic new experimental price windtunnelcourse launches sprint experimental specializes rocket sprint jet-angle plume-angle attack moment pitching nose defined ogive conical basic lift formulation 2-d 3-d circumferential increased finite-volumes 3-dimensional increasing elliptical parabolic points data x-r generating require clustering grid flexibility user-defined option series sears-haack adding transition complete boat transverse of 100 diffuser concept applying finally aerorocketcad dxf autocad using nozzle featured region nozzles number for near the lip converging-diverging underexpanded masten space mesh automatic transonic generation graphical maximum visualization equations euler takeoff xa-1 systems modeled three-dimensional inviscid solves regions

Highlighted Content Analysis

Cloud of Keywords from all content
High relevance
 

Medium relevance
 

aerocfd aerodynamics

Low relevance
 

aerocfd aerodynamics aerodrag visualcfd software aero cfd aerorocket

Very Low relevance
 
aerodrag visualcfd software aero cfd aerorocket star travel solid rocket motor wind tunnel thrust chamber pressure supersonic subsonic aerospike hypersonic airfoil drag coefficient startravel aeroisp source airplanes rockets simulation rocket airplane cfd nozzle john cipolla micro-cfd drag