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

Compton III, 1996 - Google Patents

Comparison of turbulence models for nozzle-afterbody flows with propulsive jets

Compton III, 1996

View PDF
Document ID
17025782582952321401
Author
Compton III W
Publication year

External Links

Snippet

A numerical investigation was conducted to assess the accuracy of two turbulence models when computing non-axisymmetric nozzle-afterbody flows with propulsive jets. Navier- Stokes solutions were obtained for a Convergent-divergent non-axisymmetric nozzle …
Continue reading at ntrs.nasa.gov (PDF) (other versions)

Classifications

    • 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
    • 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
    • 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
    • Y02T50/10—Drag reduction

Similar Documents

Publication Publication Date Title
Deere et al. A computational study of a dual throat fluidic thrust vectoring nozzle concept
Ding et al. An airframe/inlet integrated full-waverider vehicle design using as upgraded aerodynamic method
Compton III Comparison of turbulence models for nozzle-afterbody flows with propulsive jets
RIZK et al. Numerical prediction of the unsteady flowfield around the F-18 aircraft at large incidence
Cenko et al. PAN AIR applications to weapons carriage and separation
Kim et al. Optimal inlet shape design of N2B hybrid wing body configuration
Flores et al. Zonal Navier-Stokes methodology for flow simulation about a completeaircraft
RIZK et al. Numerical investigation of tail buffet on F-18 aircraft
Angel et al. Validation of Immersed Boundary Wall-Modelled Large Eddy Simulations with F-16XL Flight Data
Engblom Numerical Prediction of SERN Performance using WIND code
Weber et al. Three-dimensional solution of flows over wings with leading-edge vortex separation
Rizk et al. Unsteady simulation of viscous flowfield around F-18 aircraft at large incidence
Pomeroy et al. Sensitivity of Space Launch System Low-Speed Aerodynamic CFD Results to Kestrel Flow Solver Inputs
Ghaffari et al. Navier-Stokes solutions about the F/A-18 forebody-LEX configuration
Stauffer et al. A History and Commentary on Thrust/Drag Bookkeeping
Baysal et al. Interference flows past cylinder-fin-sting-cavity assemblies
William B. Compton Comparison of Turbulence Models for Nozzle-Afterbody Flows With Propulsive Jets
Long Off-design performance of hypersonic waveriders
Li et al. Integration of Engine, Plume, and CFD Analyses in Conceptual Design of Low-Boom Supersonic Aircraft
Pandya et al. Validation of inlet and exhaust boundary conditions for a Cartesian method
Malan et al. Inlet drag prediction for aircraft conceptual design
Huband et al. Numerical Simulation of an F-16A at Angle of Attack
Bui Computational Fluid Dynamics Analysis of Nozzle Plume Effects on Sonic Boom Signature
Fornasier Treatment of supersonic configurations by an updated low-order panelmethod
Shankar et al. Full potential methods for analysis/design of complex aerospace configurations