[go: up one dir, main page]
More Web Proxy on the site http://driver.im/

Baysal et al., 1992 - Google Patents

Interference flows past cylinder-fin-sting-cavity assemblies

Baysal et al., 1992

Document ID
2604793464170656571
Author
Baysal O
Fouladi K
Leung R
Sheftic J
Publication year
Publication venue
Journal of aircraft

External Links

Snippet

Interference flows past cylinder-fin-sting-cavity assemblies Page 1 JOURNAL OF AIRCRAFT Vol. 29, No. 2, March-April 1992 Interference Flows Past Cylinder-Fin-Sting-Cavity Assemblies O. Baysal* and K. Fouladit Old Dominion University, Norfolk, Virginia 23529 and RW Leungt and …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies
    • Y02T50/67Relevant aircraft propulsion technologies
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Similar Documents

Publication Publication Date Title
Yang et al. Aileron buzz simulation using an implicit multiblock aeroelastic solver
Henne Applied computational aerodynamics
Baysal et al. Interference flows past cylinder-fin-sting-cavity assemblies
Angel et al. Validation of Immersed Boundary Wall-Modelled Large Eddy Simulations with F-16XL Flight Data
CUMMINGS et al. Navier-Stokes predictions of the flowfield around the F-18 (HARV) wing and fuselage at large incidence
Koeck Computation of three‐dimensional flow using the Euler equations and a multiple‐grid scheme
Rubin et al. A review of reduced Navier-Stokes computations for compressible viscous flows
Paek et al. Computation of roll moment for projectile with wraparound fins using Euler equation
Woan et al. CFD validation of a supersonic laminar flow control concept
Compton III Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
Fouladi et al. Viscous simulation method for unsteady flows past multicomponent configurations
Fujita et al. Computational fluid dynamics evaluation of National Aerospace Laboratory experimental supersonic airplane in ascent
Shi et al. Cone-derived waverider flowfield simulation including turbulence and off-design conditions
LOMBARD et al. Numerical simulation of backward step and jet exhaust flows
Shankar et al. Full potential methods for analysis/design of complex aerospace configurations
Swanson et al. Calculation of afterbody flows with a composite velocity formulation
Baysal et al. Computing interference flows past cylinder-fin-sting assembly in andnear a cavity
Harada et al. Side force characteristics of supersonic flight vehicle equipped with asymmetric protuberance
ABDOL-HAMID et al. Supersonic Navier-Stokes simulations of turbulent afterbody flows
Hsu et al. Numerical study of vortex-dominated flows for wings at high incidence and sideslip
Carlin Jr et al. Prediction of subsonic wind tunnel mounting system interference
Miyaji et al. Tail-wing Flutter Analyses of a Balloon-based Operation Vehicle for Microgravity Experiments
Mason et al. Computational study of the F-5A forebody emphasizing directional stability
Murayama et al. Viscous Flow Computations of Aircraft with Changing Control Surface Deflection Using Unstructured Grids
Chaderjian Comparison of two Navier-Stokes codes for simulating high-incidence vortical flow