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A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application
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Computation of multi-dimensional viscous supersonic jet flow
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Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations
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A method for generating reduced order linear models of supersonic inlets
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Internal performance of a variable ramp mixed compression intake at Mach 3.05
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Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
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A comparison of approximate methods of predicting shock detachment distance for two-dimensional supersonic inlets
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Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
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The use of a lidar forward-looking turbulence sensor for mixed-compression inlet unstart avoidance and gross weight reduction on a high speed civil transport
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A method for generating reduced-order linear models of multidimensional supersonic inlets
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Minimum weight design of a generic axisymmetric inlet
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Comparison of the aeroacoustics of two small-scale supersonic inlets
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Validation of the RPLUS3D code for supersonic inlet applications involving three-dimensional shock wave boundary layer interactions
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On supersonic-inlet boundary-layer bleed flow
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Numerical simulation of supersonic flow using a new analytical bleed boundary condition
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Comparison of 3-D viscous flow computations of Mach 5 inlet with experimental data
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Analysis of inlet-compressor acoustic interactions using coupled CFD codes
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Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
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The effects of acoustic treatment on pressure disturbances from a supersonic jet in a circular duct
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Joint US/Russia TU-144 engine ground tests
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Random-choice-method solutions for two-dimensional planar and axisymmetric steady supersonic flows
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Numerical simulation of supersonic and hypersonic inlet flow fields
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An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
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Mach 10 computational study of a three-dimensional scramjet inlet flow field
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