Explore Books on
inlet flow

Numerical simulation of the flow about the F-18 HARV at high angle of attack

By Scott M. Murman

IPAC--Inlet Performance Analysis Code

By Paul J. Barnhart

A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application

By Kamlesh Kapoor

Reduction of Blade-Vortex Interaction (BVI) noise through X-force control

By Fredric H. Schmitz

Installed F/A-18 inlet flow calculations at 30 degrees angle-of-attack, a comparative study

By C. Frederic Smith

Research on a two-dimensional inlet for a supersonic V/STOL propulsion system

By J. L. Mark

Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6

By Scott Douglas Holland

Numerical simulation of supersonic and hypersonic inlet flow fields

By D. Scott McRae

Comparison of the aeroacoustics of two small-scale supersonic inlets

By Wing Ng

Control of flow separation and mixing by aerodynamic excitation

By Edward J. Rice

Theoretical and experimental study of flow-control devices for inlets of indraft wind tunnels

By James C. Ross

An experimental device for generating high frequency perturbations in supersonic wind tunnels

By Kevin J. Melcher

LDV measurements in an annular combustor model

By Dean A. Barron

Mach 10 experimental database of a three-dimensional scramjet inlet flow field

By Scott D. Holland

Inlet flow characteristics during rapid maneuvers for an F/A-18A airplane

By William G. Steenken

Numerical simulation of supersonic compression corners and hypersonic inlet flows using the RPLUS2D code

By Kamlesh Kapoor

A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow field

By Scott Douglas Holland

Design and development of an F/A-18 inlet distortion rake: a cost and time saving solution

By Andrew J. Yuhas

Mach 10 computational study of a three-dimensional scramjet inlet flow field

By Scott Douglas Holland

Development of an experimental data base to validate compressor-face boundary conditions used in unsteady inlet flow computations

By Miklos Sajben

Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10

By Scott Douglas Holland

Three dimensional compressible turbulent flow computations for a diffusing S-duct with/without vortex generators

By Soo-Yong Cho

The effects of vortex ingestion on the flow in a diffusing S-duct

By B. J. Wendt

Study of compressible flow through a rectangular-to-semiannular transition duct

By Jeffry Foster