Explore Books on
inviscid flow
1-24 of 87 Books
Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
By E. Carson Yates
Solution-adaptive Cartesian cell approach for viscous and inviscid flows
Solution-adaptive Cartesian cell approach for viscous and inviscid flows
By William J. Coirier
CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system
By Ing Chuang
Efficient gradient-based shape optimization methodology using inviscid/viscous CFD
Efficient gradient-based shape optimization methodology using inviscid/viscous CFD
By Oktay Baysal
Aeroheating predictions for X-34 using an inviscid-boundary layer method
Aeroheating predictions for X-34 using an inviscid-boundary layer method
By Christopher J. Riley
Hypersonic inviscid flow
By Wallace D. Hayes,Ronald F. Probstein
Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
The stability of two-dimensional wakes and shear-layers at high Mach numbers
The stability of two-dimensional wakes and shear-layers at high Mach numbers
By D. T. Papageorgiou
Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems
Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems
By Xiao-Yen Wang
Stable boundary conditions for Cartesian grid calculations
Stable boundary conditions for Cartesian grid calculations
By Martin J. Berger
Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows
Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows
By Osama A. Kandil
Implicit method for the computation of unsteady flows on unstructured grids
Implicit method for the computation of unsteady flows on unstructured grids
By V. Venkatakrishnan
Development of a linearized unsteady Euler analysis for turbomachinery blade rows
Development of a linearized unsteady Euler analysis for turbomachinery blade rows
By Joseph M. Verdon
On computations of the integrated space shuttle flowfield using overset grids
On computations of the integrated space shuttle flowfield using overset grids
By I.-T Chiu
Wave number selection for incompressible parallel jet flows periodic in space
Wave number selection for incompressible parallel jet flows periodic in space
By Jeffrey Hilton Miles
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
Inviscid flow computations of the orbital sciences X-34 over a Mach number range of 1.25 to 6.0
By Ramadas K. Prabhu
Wing-section optimization for supersonic viscous flows
Wing-section optimization for supersonic viscous flows
By Cem C. Item
Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
By Ramadas K. Prabhu
Numerical simulation of supersonic and hypersonic inlet flow fields
Numerical simulation of supersonic and hypersonic inlet flow fields
By D. Scott McRae
Study of the velocity gradient tensor in turbulent flow
Study of the velocity gradient tensor in turbulent flow
By Wei-Ping Cheng
A mixed volume grid approach for the Euler and Navier-Stokes equations
A mixed volume grid approach for the Euler and Navier-Stokes equations
By William John Coirier
An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
By Ramadas K. Prabhu
Evaluation of 3D inverse code using rotor 67 as test case
Evaluation of 3D inverse code using rotor 67 as test case
By T. Dang
Summary report of the orbital X-34 wing static aeroelastic study
Summary report of the orbital X-34 wing static aeroelastic study
By Ramadas K. Prabhu