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

The Resource
Supersonic flow
Resource Information

The concept

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

- Source
- nasat

## Context

Context of Supersonic flow#### Subject of

- "Supersonic Gas-Liquid Cleaning System" research project : final summary report under NASA Cooperative Agreement no.: NCC10-0010
- A multi-domain spectral method for supersonic reactive flows
- A numerical method for solving the three-dimensional parabolized Navier-Stokes equations
- A preliminary design study of supersonic through-flow fan inlets
- Aeroacoustics of supersonic jet flows from contoured and solid-porous conical plug-nozzles
- Aerodynamic shape optimization directed toward a supersonic transport using sensitivity analysis : final report for the period ended August 15, 1995
- An analysis of supersonic flows with low-Reynolds number compressible two-equation turbulence models using LU finite volume implicit numerical techniques
- An assessment of the adaptive unstructured tetrahedral grid, Euler flow solver code FELISA
- An asymptomatic theory of supersonic propeller noise
- An asymptotic analysis of supersonic reacting mixing layers
- An asymptotic analysis of supersonic reacting mixing layers
- An edge-based solution-adaptive method applied to the AIRPLANE code
- An efficient parallel algorithm for the simulation of three-dimensional compressible transition on a 20 processor Flex/32 multicomputer
- An experimental study of turbulent skin friction reduction in supersonic flow using a microblowing technique
- An extended Lagrangian method
- Analysis and design of numerical schemes for gas dynamics 1 : artificial diffusion, upwind biasing, limiters and their effect on accuracy and multigrid convergence
- Application of a Runge-Kutta scheme for high-speed inviscid internal flows
- Application of a two-dimensional unsteady viscous analysis code to a supersonic throughflow fan stage
- Boundary layer transition in the leading edge region of a swept cylinder in high speed flow
- Comparison of 3D computation and experiment for non-axisymmetric nozzles
- Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating
- Computation of Navier-Stokes equations for three-dimensional flow separation
- Computation of asymmetric supersonic flows around cones at large incidence : final report
- Computational aeroservoelastic analysis with an Euler-based unsteady flow solver : NASA-Ames university consortium cooperative agreement no. NCC2-5105, final research summary for the period: 1 November 1994 - 31 January 1997
- Computational analysis of a low-boom supersonic inlet
- Development of a laser-induced heat flux technique for measurement of convective heat transfer coefficients in a supersonic flowfield
- Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle : final report
- Development of an upwind, finite-volume code with finite-rate chemistry
- Doppler global velocimetry at NASA Glenn Research Center : system discussion and results
- Embedded function methods for compressible high speed turbulent flow : final report
- Entropy stable wall boundary conditions for the compressible Navier-Stokes equations
- Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows
- Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16
- Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
- Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16
- Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 : final report
- F-16XL-2 supersonic laminar flow control flight test experiment
- Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer
- Factors influencing pitot probe centerline displacement in a turbulent supersonic boundary layer
- Final report for NASA Ames cooperative agreement, NCC2-5049
- Final report for NASA Ames cooperative agreement, NCC2-5049
- Final report for NASA grant NAGW-1514, titled, magnetic field waves at Uranus, to the Bartol Research Institute of the University of Delaware, administered under the auspices of the Uranus Data Analysis Program
- First derivatives of flow quantities behind two-dimensional, nonuniform supersonic flow over a convex corner
- Flow characteristics in boundary layer bleed slots with plenum
- Flow matching results of an MHD energy bypass system on a supersonic turbojet engine using the numerical propulsion system simulation (NPSS) environment
- Flow visualization by elastic light scattering in the boundary layer of a supersonic flow
- In-flight imaging of transverse gas jets injected into transonic and supersonic crossflows : design and development
- Inflow/outflow boundary conditions with application to FUN3D
- Inlet flowfield investigation, Part II., Computation of the flow about a supercruise forebody at supersonic speeds
- Instantaneous 2D velocity and temperatire measurements in high speed flows based on spectrally resolved molecular Rayleigh scattering
- Instrumentation development for study of Reynolds analogy in reacting flows
- Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport
- Investigation of chemically-reacting supersonic internal flows
- Investigation of flow separation in a transonic-fan linear cascade using visualization methods
- Investigation of flow separation in a transonic-fan linear cascade using visualization methods
- Investigation of mixing a supersonic stream with the flow downstream of a wedge : NCC2-5190 final report
- Investigation of parabolic computational techniques for internal high-speed viscous flows
- Investigation of ramp injectors for supersonic mixing enhancement
- Investigation of supersonic chemically reacting and radiating channel flow
- Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors
- Measurement and computation of supersonic flow in a lobed diffuser-mixer for trapped vortex combustors
- Methodology for sensitivity analysis, approximate analysis, and design optimization in CFD for multidisciplinary applications : final report for the period ended December 31, 1995
- NASA Glenn 1-by 1-foot supersonic wind tunnel user manual
- NASA Glenn 1-by 1-foot supersonic wind tunnel user manual
- Nonlinear interaction between a pair of oblique modes in a supersonic mixing layer : long wave limit
- Nonlinear potential analysis techniques for supersonic aerodynamic design
- Numerical calculations of shock-wave/boundary-layer flow interactions
- Numerical simulation of jet aerodynamics using the three-dimensional Navier-Stokes code PAB3D
- Numerical simulation of shock/turbulent boundary layer interaction : final year report for NASA grant NAG-1-1472
- Numerical simulation of stability and stabiity control of high speed compressible rotating couette flow : final report for NASA grant NAG-1-1103
- Numerical simulation of supersonic flow using a new analytical bleed boundary condition
- Optical measurements of fluctuating temperatures in a supersonic turbulent flow using one- and two-photon, laser-induced fluorescence
- Optical techniques for determination of normal shock position in supersonic flows for aerospace applications
- Optical techniques for shock visualization and detection
- Parallelization of a parabolized Navier-Stokes solver with a design optimizer : 34th AIAA Aerospace Sciences Meeting and Exhibit
- Photodiagnostics of turbulent flows using laser-induced fluorescence : final report
- Potential flow downstream of the heliospheric terminal schock : a non-spherical schock / Steven Nerney and Steven T. Suess
- RNS applications for interacting sub- and supersonic flows : final report, NASA grant no. NAG1-1553, 11/19/93-5/18/97
- STARS : an integrated general-purpose finite element structural, aeroelastic, and aeroservoelastic analysis computer program
- Seeding for laser velocimetry in confined supersonic flows with shocks
- Seeding for laser velocimetry in confined supersonic flows with shocks
- Shear flow control of cold and heated rectangular jets by mechanical tabs
- Study of injection of helium into supersonic air flow using Rayleigh scattering
- Study of injection of helium into supersonic air flow using Rayleigh scattering
- Supersonic flow computations for an ASTOVL aircraft configuration : phase 2, part 2
- Supersonic laminar flow control research : NASA grant no. NAG 2-881, final report, January 1994 - June 1996
- Supersonic laminar flow control research : final report, July 1994-June 1996
- Supersonic laminar flow control research : semiannual report #2
- Supersonic laminar flow control research : semiannual report #4, July 1995 - December 1995
- Supersonic reacting internal flow fields
- Supersonic wing and wing-body shape optimization using an adjoint formulation
- Surface documentation of a 3-D supersonic, shock-wave-boundary layer interaction
- The Kirchhoff formulas for moving surfaces in aeroacoustics : the subsonic and supersonic cases
- The effect of three-dimensional freestream disturbances on the supersonic flow past a wedge : NASA contract no. NAS1-19480
- The inviscid axisymmetric stability of the supersonic flow along a circular cylinder
- The inviscid stability of supersonic flow past a sharp cone
- Theoretical and experimental flow fields for a supersonic cruise fighter forebody
- TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations : theory document
- TranAir, a full-potential, solution-adaptive, rectangular grid code for predicting subsonic, transonic, and supersonic flows about arbitrary configurations : user's manual
- USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
- USSAERO version D computer program development using ANSI standard FORTRAN 77 and DI-3000 graphics
- Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations
- User's guide for NASCRIN--a vectorized code for calculating two-dimensional supersonic internal flow fields
- VORCAM : a computer program for calculating vortex lift effect of cambered wings by the suction analogy
- Validation of WIND for a series of inlet flows
- Validation of WIND for a series of inlet flows
- Verification assessment of flow boundary conditions for CFD analysis of supersonic inlet flows
- Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
- Wind-US code contributions to the first AIAA Shock Boundary Layer Interaction Prediction Workshop
- Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes
- Wing-section optimization for supersonic viscous flow : [abstract]
- Wing-section optimization for supersonic viscous flows : abstract

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