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hypersonics

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View Development of the X-33 aerodynamic uncertainty model By Brent R. Cobleigh

Development of the X-33 aerodynamic uncertainty model

Development of the X-33 aerodynamic uncertainty model

By Brent R. Cobleigh

View The X-33 extended flight test range By Dale A. Mackall

The X-33 extended flight test range

The X-33 extended flight test range

By Dale A. Mackall

View Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration By W. Pelham Phillips

Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration

Subsonic-to-hypersonic aerodynamic characteristics for a winged, circular-body, single-stage-to-orbit spacecraft configuration

By W. Pelham Phillips

View Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel By Glen P. Doggett

Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel

Hypersonic boundary-layer stability experiments on a flared-cone model at angle of attack in a quiet wind tunnel

By Glen P. Doggett

View Aeroheating predictions for X-34 using an inviscid-boundary layer method By Christopher J. Riley

Aeroheating predictions for X-34 using an inviscid-boundary layer method

Aeroheating predictions for X-34 using an inviscid-boundary layer method

By Christopher J. Riley

View CFD for hypersonic propulsion By Louis A. Povinelli

CFD for hypersonic propulsion

CFD for hypersonic propulsion

By Louis A. Povinelli

View Thermal and structural assessments of a ceramic wafer seal in hypersonic engines By Michael T. Tong

Thermal and structural assessments of a ceramic wafer seal in hypersonic engines

Thermal and structural assessments of a ceramic wafer seal in hypersonic engines

By Michael T. Tong

View An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies By Irina G. Brykina

An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies

An approximate axisymmetric viscous shock layer aeroheating method for three-dimensional bodies

By Irina G. Brykina

View An outlook on hypersonic flight By Griffin Y. Anderson

An outlook on hypersonic flight

An outlook on hypersonic flight

By Griffin Y. Anderson

View Hypersonic boundary-layer transition for X-33 phase II vehicle By R. A. Thompson

Hypersonic boundary-layer transition for X-33 phase II vehicle

Hypersonic boundary-layer transition for X-33 phase II vehicle

By R. A. Thompson

View A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients By Stephen A. Whitmore

A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients

A dynamic response model for pressure sensors in continuum and high Knudsen number flows with large temperature gradients

By Stephen A. Whitmore

View Internal performance predictions for Langley scramjet engine module By S. Z. Pinckney

Internal performance predictions for Langley scramjet engine module

Internal performance predictions for Langley scramjet engine module

By S. Z. Pinckney

View The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts By Alexander M. Starik

The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts

The kinetic nonequilibrium processes in the internal flow and in the plume of subsonic and supersonic aircrafts

By Alexander M. Starik

View Morphology of a standing oblique detonation wave By David T. Pratt

Morphology of a standing oblique detonation wave

Morphology of a standing oblique detonation wave

By David T. Pratt

View Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0 By Ira J. Walker

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

Experimental aerodynamic characteristics of a generic hypersonic accelerator configuration at Mach numbers 1.5 and 2.0

By Ira J. Walker

View An approximate Riemann solver for thermal and chemical nonequilibrium flows By Ramadas K. Prabhu

An approximate Riemann solver for thermal and chemical nonequilibrium flows

An approximate Riemann solver for thermal and chemical nonequilibrium flows

By Ramadas K. Prabhu

View Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications By N. Sinha

Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications

Inclusion of chemical kinetics into beam-warming based PNS model for hypersonic propulsion applications

By N. Sinha

View Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65 degrees By Edward R. Hartmann

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65 degrees

Mach 6 experimental and theoretical stability and performance of a cruciform missile at angles of attack up to 65 degrees

By Edward R. Hartmann

View Airbreathing hypersonic systems focus at NASA Langley Research Center By James L. Hunt

Airbreathing hypersonic systems focus at NASA Langley Research Center

Airbreathing hypersonic systems focus at NASA Langley Research Center

By James L. Hunt

View Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel By R. P. Mason

Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel

Pitot-pressure measurements in the nozzle of the UTIAS 11" x 15" hypersonic shock tunnel

By R. P. Mason

View Summary of shock tunnel development and application to hypersonic research By Abraham Hertzberg

Summary of shock tunnel development and application to hypersonic research

Summary of shock tunnel development and application to hypersonic research

By Abraham Hertzberg

View Hypersonic turbulent boundary-layer and free shear database By Gary S. Settles

Hypersonic turbulent boundary-layer and free shear database

Hypersonic turbulent boundary-layer and free shear database

By Gary S. Settles

View Demonstration of oblique detonation wave for hypersonic propulsion By Takashi Nakamura

Demonstration of oblique detonation wave for hypersonic propulsion

Demonstration of oblique detonation wave for hypersonic propulsion

By Takashi Nakamura

View Systems challenges for hypersonic vehicles By James L. Hunt

Systems challenges for hypersonic vehicles

Systems challenges for hypersonic vehicles

By James L. Hunt