Nothing Special   »   [go: up one dir, main page]

Viti et al., 2004 - Google Patents

Jet interaction with a primary jet and an array of smaller jets

Viti et al., 2004

Document ID
18281090719525940694
Author
Viti V
Wallis S
Schetz J
Neel R
Bowersox R
Publication year
Publication venue
AIAA journal

External Links

Snippet

Jet Interaction with a Primary Jet and an Array of Smaller Jets Page 1 AIAA JOURNAL Vol. 42, No. 7, July 2004 Jet Interaction with a Primary Jet and an Array of Smaller Jets Valerio Viti, ∗ Scott Wallis,† and Joseph A. Schetz‡ Virginia Polytechnic Institute and State University, Blacksburg …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies
    • Y02T50/67—Relevant aircraft propulsion technologies
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50—Computer-aided design
    • G06F17/5009—Computer-aided design using simulation
    • G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods

Similar Documents

Publication Publication Date Title
Huang et al. Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows
Titchener et al. Shock wave/boundary-layer interaction control using a combination of vortex generators and bleed
Kawai et al. Computational study of a supersonic base flow using hybrid turbulence methodology
Pudsey et al. Behavior of multiple-jet interactions in a hypersonic boundary layer
Deere et al. A computational study of a dual throat fluidic thrust vectoring nozzle concept
Koklu Effect of a Coanda extension on the performance of a sweeping-jet actuator
Zhang et al. Control of shock/boundary-layer interaction for hypersonic inlets by highly swept microramps
Jin et al. The effects of Maxwellian accommodation coefficient and free-stream Knudsen number on rarefied hypersonic cavity flows
Mele et al. Drag bookkeeping on an aircraft with riblets and NLF control
Srinivasan et al. Transverse injection through diamond and circular ports into a Mach 5.0 freestream
Viti et al. Jet interaction with a primary jet and an array of smaller jets
Pelletier et al. Wall roughness effects on combustion development in confined supersonic flow
Deere PAB3D simulations of a nozzle with fluidic injection for yaw thrust-vector control
Kawai et al. Computational study of a supersonic base flow using LES/RANS hybrid methodology
Eklund et al. Study of a supersonic combustor employing an aerodynamic ramp pilot injector
Rana et al. Dynamics of sonic hydrogen jet injection and mixing inside scramjet combustor
Graham et al. Numerical simulation of lateral control jets
Srinivasan et al. Simulation of transverse gaseous injection through diamond ports into supersonic freestream
Zhen et al. Numerical investigation on jet interaction with a compression ramp
Séror et al. Compressible Turbulence Model consistency for separated high-speed flow regimes
Mrozinski et al. Numerical and experimental analysis of a hypersonic variable geometry inlet
Monat et al. Suction and pulsed blowing applied to local separation downstream of slat cutout
Viviani et al. Effect of finite rate chemical models on the aerothermodynamics of reentry capsules
Bui CFD Analysis of the Nozzle Jet Plume Effects on Sonic Boom Signature
Lüdeke et al. Simulation of streamwise vortices at the flaps of re-entry vehicles