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

The Resource
Engine inlets
Resource Information

The concept

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

- Source
- nasat

## Context

Context of Engine inlets#### Subject of

- 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics
- A numerical analysis applied to high angle of attack three-dimensional inlets
- A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92
- Acoustic mode measurements in the inlet of a model turbofan using a continuously rotating rake
- Active control of fan noise-feasibility study : flyover system noise studies
- Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model
- Air intakes for a probative missile of rocket ramjet
- An investigation of bleed configurations and their effect on shock wave/boundary layer interactions : final report
- Application of CFD to the analysis and design of high-speed inlets : final report
- Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet
- Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet
- Collection efficiency and ice accretion calculations for a sphere, a swept MS(1)-317 wing, a swept NACA-0012 wing tip, an axisymmetric inlet, and a Boeing 737-300 inlet
- Combined cycle engine large-scale inlet for mode transition experiments : system identification rack hardware design
- Comparison of the aeroacoustics of two small-scale supersonic inlets : final technical report, NASA contract #--NAG 3-1539
- Computational analysis in support of the SSTO flowpath test
- Computational analysis of a low-boom supersonic inlet
- Control of flow separation and mixing by aerodynamic excitation
- Design and development of an F/A-18 inlet distortion rake : a cost and time saving solution
- Determination of shed ice particle size using high speed digital imaging
- Development and characterization testing of an air pulsation valve for a pulse detonation engine supersonic parametric inlet test section
- Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations : a final technical report for NASA-LeRC grant NAG-1781
- Dynamic inlet distortion prediction with a combined computational fluid dynamics and distortion synthesis approach
- Dynamic testing of the NASA Hypersonic Project combined cycle engine testbed for mode transition experiments
- Effects of initial conditions on a single jet in crossflow
- Evaluation of panel code predictions with experimental results of inlet performance for a 17-inch ducted prop/fan simulator operating at mach 0.2
- Experimental investigation of inlet-combustor isolators for a dual-mode scramjet at a Mach number of 4
- Experimental investigation of the inlet deflector configuration variation in the flow field at mach 1.9 : final report
- Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet
- Experimental investigation of water droplet impingement on airfoils, finite wings, and an S-duct engine inlet
- Fan noise prediction assessment
- Fan noise prediction system development : source/radiation field coupling and workstation conversion for the acoustic radiation code
- Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft
- Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design
- Finite difference time marching in the frequency domain : a parabolic formulation for aircraft acoustic nacelle design
- Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
- Flow through a rectangular-to-semiannular diffusing transition duct
- High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion
- Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion
- IPAC--Inlet Performance Analysis Code
- Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
- Improved finite element modeling of the turbofan engine inlet radiation problem
- Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack
- Investigation of "6X" scramjet inlet configurations
- Mach 10 experimental database of a three-dimensional scramjet inlet flow field
- Mach 5 inlet CFD and experimental results
- Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines
- Multigrid methods for aerodynamic problems in complex geometries : final report
- NASA Lewis Propulsion Systems Laboratory customer guide manual
- Nearly interactive Parabolized Navier-Stokes solver for high speed forebody and inlet flows
- Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
- Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
- PARC3D calculations of the F/A-18A HARV inlet vortex generators
- Performance study for inlet installations
- Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
- Rocket-based combined cycle engine technology development : inlet CFD validation and application
- Rocket-based combined cycle engine technology development : inlet CFD validation and application
- SSME fuelside preburner two-dimensional analysis
- Shock position control for mode transition in a turbine based combined cycle engine inlet model
- Study of compressible flow through a rectangular-to-semiannular transition duct
- Testing of the NASA Hypersonics project's Combined Cycle Engine Large Scale Inlet Mode Transition Experiment (CCE LIMX)
- Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators
- Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
- Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow
- Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

## Embed (Experimental)

### Settings

Select options that apply then copy and paste the RDF/HTML data fragment to include in your application

Embed this data in a secure (HTTPS) page:

Layout options:

Include data citation:

<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.houstonlibrary.org/resource/KNI9NeClJWU/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.houstonlibrary.org/resource/KNI9NeClJWU/">Engine inlets</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.houstonlibrary.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.houstonlibrary.org/">Houston Public Library</a></span></span></span></span></div>

Note: Adjust the width and height settings defined in the RDF/HTML code fragment to best match your requirements

### Preview

## Cite Data - Experimental

### Data Citation of the Concept Engine inlets

Copy and paste the following RDF/HTML data fragment to cite this resource

`<div class="citation" vocab="http://schema.org/"><i class="fa fa-external-link-square fa-fw"></i> Data from <span resource="http://link.houstonlibrary.org/resource/KNI9NeClJWU/" typeof="CategoryCode http://bibfra.me/vocab/lite/Concept"><span property="name http://bibfra.me/vocab/lite/label"><a href="http://link.houstonlibrary.org/resource/KNI9NeClJWU/">Engine inlets</a></span> - <span property="potentialAction" typeOf="OrganizeAction"><span property="agent" typeof="LibrarySystem http://library.link/vocab/LibrarySystem" resource="http://link.houstonlibrary.org/"><span property="name http://bibfra.me/vocab/lite/label"><a property="url" href="http://link.houstonlibrary.org/">Houston Public Library</a></span></span></span></span></div>`