#
Inviscid flow
Resource Information
The concept ** Inviscid flow** represents the subject, aboutness, idea or notion of resources found in **Houston Public Library**.

The Resource
Inviscid flow
Resource Information

The concept

**Inviscid flow**represents the subject, aboutness, idea or notion of resources found in**Houston Public Library**.- Label
- Inviscid flow

- Source
- nasat

## Context

Context of Inviscid flow#### Subject of

- 11 foot Unitary Plan tunnel facility optical improvement large window analysis
- A Modified lifted line theory for wing-propeller interference : progress report for the period June 1 to September 30, 1983
- A high order discontinuous Galerkin method for 2D incompressible flows
- A mixed volume grid approach for the Euler and Navier-Stokes equations
- A new finite element approach for prediction of aerothermal loads--progress in inviscid flow computations
- A numerical method for solving the three-dimensional parabolized Navier-Stokes equations
- A numerical simulation of the inviscid flow through a counter-rotating propeller
- A viscous-inviscid interactive procedure for rotational flow in cascades of two dimensional airfoils of arbitrary shape : final report
- ALESEP, Part II : a computer program for the analysis of leading edge separation bubbles on infinite swept wings
- Advanced space propulsion system flowfield modeling : final report : contract NAS8-40845
- Aerodynamic design optimization on unstructured grids with a continuous adjoint formulation
- Aerodynamics of engine-airframe interaction : final report
- Aeroelastic calculations using CFD for a typical business jet model
- An approximate Riemann solver for thermal and chemical nonequilibrium flows
- An approximate method for calculating three-dimensional inviscid hypersonic flow fields
- An axisymmetric analog two-layer convective heating procedure with application to the evaluation of space shuttle orbiter wing leading edge and windeward surface heating
- An improved viscid/inviscid interaction procedure for transonic flow over airfoils
- An inviscid computational study of an X-33 configuration at hypersonic speeds
- An inviscid computational study of three '07 Mars lander aeroshell configurations over a Mach number range of 2.3 to 4.5
- Analysis and mitigation of numerical dissipation in inviscid and viscid computation of vortex-dominated flows : final report for the period February 1988 to November 1988
- Analysis of inviscid and viscous flows in cascades with an explicit multiple-grid algorithm
- Analysis of transitional separation bubbles on infinite swept wings
- Analytical determination of propeller performance degradation due to ice accretion
- Analytical determination of propeller performance degradation due to ice accretion
- Application of a Runge-Kutta scheme for high-speed inviscid internal flows
- Application of a third order upwind scheme to viscous flow over clean and iced wings : 32nd Aerospace Sciences Meeting & Exhibit, January 10-13, 1994/Reno, NV
- Application of the space-time conservation element and solution element method to one-dimensional advection-diffusion problems
- Assessment of three-dimensional inviscid codes and loss calculations for turbine aerodynamic computations
- CFD study of turbo-Ramjet interactions in hypersonic airbreathing propulsion system : final report : under contract NAG3-1500
- Calculation of laminar heating rates on three-dimensional configurations using the axisymmetric analogue
- Calculation of viscous effects on transonic flow for oscillating airfoils and comparisons with experiment
- Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading
- Comparison of secondary flows predicted by a viscous code and inviscid code with experimental data for a turning duct
- Computational study of a McDonnell Douglas single-stage-to-orbit vehicle concept for aerodynamic analysis
- Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed
- Development of a linearized unsteady Euler analysis for turbomachinery blade rows
- Efficient gradient-based shape optimization methodology using inviscid/viscous CFD : summary of research report for the period of March 9, 1995 to March 8, 1997, grant# NCC-1-211
- Efficient self-consistent viscous-inviscid solutions for unsteady transonic flow
- Enhanced viscous flow drag reduction using acoustic excitation : final report
- Entropy condtion satisfying approximations for the full potential equations of transonic flow
- Entropy jump across an inviscid shock wave
- Euler technology assessment : SPLITFLOW code applications for stability and control analysis on an advanced fighter model employing innovative control concepts
- Evaluation of 3D inverse code using rotor 67 as test case : final report
- Finite element methods of analysis for 3d inviscid compressible flows : final report for the period 1 December 1989, 30 November 1990
- GRUMFOIL, a computer code for the viscous transonic flow over airfoils
- Impact of an exhaust throat on semi-idealized rotating detonation engine performance
- Implementation of advanced two equation turbulence models in the USM3D unstructured flow solver
- Implicit method for the computation of unsteady flows on unstructured grids
- Integral-equation methods in steady and unsteady subsonic, transonic and supersonic aerodynamics for interdisciplinary design
- Interface behavior of a multi-layer fluid ocnfiguration subject to acceleration in a microgravity environment : supplement I
- Inviscid flow computations of several aeroshell configurations for a '07 Mars lander
- 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 shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees
- Inviscid flow computations of two '07 Mars Lander aeroshell configurations over Mach number range of 2 to 24
- Inviscid spatial stability of a compressible mixing layer, Part II, The flame sheet model
- Inviscid spatial stability of a compressible mixing layer, Part III, Effect of thermodynamics
- Large perturbation flow field analysis and simulation for supersonic inlets : final report
- Methodology for simulation of unsteady flows to determine the time-dependent interference between stationary and moving boundaries : [abstract
- Multigrid calculation of three-dimensional turbomachinery flows
- Multigrid methods for aerodynamic problems in complex geometries : final report
- Multigrid solution strategies for adaptive meshing problems
- Nonlinear effects on the natural modes of oscillation of a finite length inviscid fluid column : supplement II
- Nonlinear potential analysis techniques for supersonic/hypersonic aerodynamic design
- Numerical flux formulas for the Euler and Navier-Stokes equations
- Numerical simulation of supersonic and hypersonic inlet flow fields : final report
- Numerical simulation of vitiation effects on a hydrogen-fueled dual-mode scramjet
- Numerical solution of the incompressible Navier-Stokes equations
- Numerical speed of sound and its application to schemes for all speeds
- On computations of the integrated space shuttle flowfield using overset grids : final report
- On similarity solutions of a boundary layer problem with an upstream moving wall
- Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Pressure updating methods for the steady-state fluid equations
- Progress in grid generation : from chimera to DRAGON grids
- Progress toward the development of an airfcraft icing analysis capability
- Simple numerical method for predicting steady compressible flows : progress report for the period ended November 14, 1986
- Solution-adaptive Cartesian cell approach for viscous and inviscid flows
- Some approaches towards constructing optimally efficient multigrid solvers for the inviscid flow equations
- Spectral methods in fluid dynamics
- Stable boundary conditions for Cartesian grid calculations
- Structure of the small amplitude motion on transversely sheared mean flows
- Study of the velocity gradient tensor in turbulent flow
- Summary report of the orbital X-34 wing static aeroelastic study
- Supercomputer implementation of finite element algorithms for high speed compressible flows : progress report for the period ended June 30, 1986
- The calculation of the mass moment of inertia of a fluid in a rotating rectangular tank
- The design/analysis of flows through turbomachinery : a viscous/inviscid approach
- The inviscid stability of supersonic flow past a sharp cone
- The nonlinear evolution of inviscid Gortler vortices in three-dimensional boundary layers
- The stability of two-dimensional wakes and shear-layers at high Mach numbers
- Theory of finite disturbances in a centrifuglal compression system with a vaneless radial diffuser
- Towards enhancing and delaying disturbances in free shear flows
- Unsteady aerodynamics : subsonic compressible inviscid case
- Unstructured grid Euler method assessment for longitudinal and lateral/directional stability analysis of the HSR Reference H configuration at transonic speeds
- Unstructured grid Euler method assessment for longitudinal and lateral/directional stability analysis of the HSR Reference H configuration at transonic speeds
- Unstructured grid methods for the simulation of 3D transient flows : final report for the period, 1 January 1992 - 31 December 1993
- Validation of viscous and inviscid computational methods for turbomachinery components
- Viscous wing theory development : final report
- WIND : computer program for calculation of three-dimensional potential compressible flow about wind turbine rotor blades
- Wave number selection for incompressible parallel jet flows periodic in space
- Wave number selection for incompressible parallel jet flows periodic in space
- Wing-section optimization for supersonic viscous flows : abstract
- Zonally averaged model of dynamics, chemistry and radiation for the atmosphere : semiannual status report for the period June 1, 1985 to November 30, 1985

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