1-24 of 38 Books
IPAC--Inlet Performance Analysis Code
IPAC--Inlet Performance Analysis Code
By Paul J. Barnhart
Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations
Development of a low-Reynolds number, nonlinear [kappa-epsilon] model for the reduced Navier-Stokes equations
By David A. Boger
Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems
By K. B. Kontos
Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
Finite element elastic-plastic-creep and cyclic life analysis of a cowl lip
By V. K. Arya
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
By Kenneth J. Baumeister
Rocket-based combined cycle engine technology development
Rocket-based combined cycle engine technology development
By J. R. DeBonis
NASA Lewis Propulsion Systems Laboratory customer guide manual
NASA Lewis Propulsion Systems Laboratory customer guide manual
By Ronald H. Soeder
An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
An investigation of bleed configurations and their effect on shock wave/boundary layer interactions
By A. Hamed
Comparison of the aeroacoustics of two small-scale supersonic inlets
Comparison of the aeroacoustics of two small-scale supersonic inlets
By Wing Ng
Finite difference time marching in the frequency domain
Finite difference time marching in the frequency domain
By Kenneth J. Baumeister
3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By M. Mizukami
Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet
Collection efficiency and ice accretion calculations for a Boeing 737-300 inlet
By Colin 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
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
By Colin S. Bidwell
Control of flow separation and mixing by aerodynamic excitation
Control of flow separation and mixing by aerodynamic excitation
By Edward J. Rice
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
Mach 10 experimental database of a three-dimensional scramjet inlet flow field
By Scott D. Holland
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
Wind-tunnel blockage and actuation systems test of a two-dimensional scramjet inlet unstart model at Mach 6
By Scott Douglas Holland
Performance study for inlet installations
Performance study for inlet installations
By D. C. Bingaman
3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
Multigrid methods for aerodynamic problems in complex geometries
Multigrid methods for aerodynamic problems in complex geometries
By D. A. Caughey
Application of CFD to the analysis and design of high-speed inlets
Application of CFD to the analysis and design of high-speed inlets
By William C. Rose
Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
Numerical analysis of the trailblazer inlet flowfield for hypersonic Mach numbers
By C. J. Steffen
Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
Prediction of wind tunnel effects on the installed F/A-18A inlet flow field at high angles-of-attack
By Crawford F. Smith
A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics
A design strategy for the use of vortex generators to manage inlet-engine distortion using computational fluid dynamics
By Bernhard H. Anderson
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
By Richard J. Re