Engine Inlets

87 books
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 inletColin S. Bidwell

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

Colin S. Bidwell

1995No page data
Numerical calculation of scramjet inlet flowTomiko Ishiguro
⏱ 29m

Numerical calculation of scramjet inlet flow

Tomiko Ishiguro

199229 pp.
Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbersC. J. Steffen

Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers

C. J. Steffen

1999No page data
Study of compressible flow through a rectangular-to-semiannular transition ductUnknown Author

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

Unknown Author

1995No page data
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6Scott D. Holland

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

Scott D. Holland

1994No page data
Effects of initial conditions on a single jet in crossflowD. S. Liscinsky

Effects of initial conditions on a single jet in crossflow

D. S. Liscinsky

1995No page data
An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applicationsPaul L. McDill

An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications

Paul L. McDill

1986No page data
Control of flow separation and mixing by aerodynamic excitationEdward J. Rice
⏱ 11m

Control of flow separation and mixing by aerodynamic excitation

Edward J. Rice

199011 pp.
Finite element elastic-plastic-creep and cyclic life analysis of a cowl lipV. K. Arya

Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip

V. K. Arya

1990No page data
Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flowKenneth J. Baumeister

Time-dependent parabolic finite difference formulation for harmonic sound propagation in a two-dimensional duct with flow

Kenneth J. Baumeister

1996No page data
A study of sand waves in the Panama City, Florida, entrance channelW. Jeff Lillycrop
⏱ 58m

A study of sand waves in the Panama City, Florida, entrance channel

W. Jeff Lillycrop

198958 pp.
Shock-tunnel combustor testing for hypersonic vehiclesMark Loomis

Shock-tunnel combustor testing for hypersonic vehicles

Mark Loomis

1994No page data
Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraftChoon Sooi Tan

Final technical report on grant NAG3-1567 entitled Inlet distortion in engines on VSTOL aircraft

Choon Sooi Tan

1994No page data
A performance map for ideal air breathing pulse detonation enginesDaniel E. Paxon

A performance map for ideal air breathing pulse detonation engines

Daniel E. Paxon

2001No page data
A computational and experimental investigation of a three-dimensional hypersonic scramjet inlet flow fieldScott Douglas Holland

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

Scott Douglas Holland

1991No page data
High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestionBobby L. Berrier
⏱ 2h 45m

High Reynolds number investigation of a flush-mounted, S-duct inlet with large amounts of boundary layer ingestion

Bobby L. Berrier

2005165 pp.
Rocket-based combined cycle engine technology developmentJ. R. DeBonis

Rocket-based combined cycle engine technology development

J. R. DeBonis

1996No page data
A preliminary design study of supersonic through-flow fan inletsPaul J. Barnhart

A preliminary design study of supersonic through-flow fan inlets

Paul J. Barnhart

1988No page data
Internal aerodynamics of a generic three-dimensional scramjet inlet at Mach 10Scott Douglas Holland

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

Scott Douglas Holland

1995No page data
Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan enginesD. E. Cicon

Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines

D. E. Cicon

1995No page data
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