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aerothermodynamics

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View Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields By Leland A. Carlson

Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields

Nonequilibrium radiation and chemistry models for aerocapture vehicle flowfields

By Leland A. Carlson

View Basics Of Aerothermodynamics By Ernst Heinrich Hirschel
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Basics Of Aerothermodynamics

By Ernst Heinrich Hirschel

View Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces By William L. Ko

Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces

Open-mode debonding analysis of curved sandwich panels subjected to heating and cryogenic cooling on opposite faces

By William L. Ko

View Navier-Stokes analysis of turbine blade heat transfer By Robert J. Boyle

Navier-Stokes analysis of turbine blade heat transfer

Navier-Stokes analysis of turbine blade heat transfer

By Robert J. Boyle

View Finite element thermo-viscoplastic analysis of aerospace structures By Ajay K. Pandey

Finite element thermo-viscoplastic analysis of aerospace structures

Finite element thermo-viscoplastic analysis of aerospace structures

By Ajay K. Pandey

View Aerodynamic Data of Space Vehicles By Claus Weiland
Cover of Aerodynamic Data of Space Vehicles by claus weiland

Aerodynamic Data of Space Vehicles

By Claus Weiland

View Aerothermodynamics of gas turbine and rocket propulsion By Gordon C. Oates
Cover of Aerothermodynamics of gas turbine and rocket propulsion by gordon c. oates

Aerothermodynamics of gas turbine and rocket propulsion

By Gordon C. Oates

View Recent advances in aerothermochemistry By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

Recent advances in aerothermochemistry

Recent advances in aerothermochemistry

By North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development.

View Aerothermal environment in chordwise gaps between split elevons at Mach 6.8 By L. Roane Hunt

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8

Aerothermal environment in chordwise gaps between split elevons at Mach 6.8

By L. Roane Hunt

View Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3 By Robert L. Stallings

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3

Wind-tunnel measurements and comparison with flight of the boundary layer and heat transfer on a hollow cylinder at Mach 3

By Robert L. Stallings

View Real-gas flow properties for NASA Langley Research Center Aerothermodynamic Facilities Complex wind tunnels By Brian R. Hollis

Real-gas flow properties for NASA Langley Research Center Aerothermodynamic Facilities Complex wind tunnels

Real-gas flow properties for NASA Langley Research Center Aerothermodynamic Facilities Complex wind tunnels

By Brian R. Hollis

View Introduction to Aircraft Thermal Management By Mark Ahlers

Introduction to Aircraft Thermal Management

Introduction to Aircraft Thermal Management

By Mark Ahlers

View Aerothermodynamics of aircraft engine components By Gordon C. Oates
Cover of Aerothermodynamics of aircraft engine components by gordon c. oates

Aerothermodynamics of aircraft engine components

By Gordon C. Oates

View A short time response stagnation temperature probe By R. A. East

A short time response stagnation temperature probe

A short time response stagnation temperature probe

By R. A. East

View Table and charts of equilibrium normal-shock properties for pure hydrogen with velocities to 70 km/sec By Charles G. Miller

Table and charts of equilibrium normal-shock properties for pure hydrogen with velocities to 70 km/sec

Table and charts of equilibrium normal-shock properties for pure hydrogen with velocities to 70 km/sec

By Charles G. Miller

View Thermal structures By Earl A. Thornton

Thermal structures

Thermal structures

By Earl A. Thornton

View Table and charts of equilibrium normal shock and shock-tube properties for pure argon with velocities to 18 km/sec By Charles G. Miller

Table and charts of equilibrium normal shock and shock-tube properties for pure argon with velocities to 18 km/sec

Table and charts of equilibrium normal shock and shock-tube properties for pure argon with velocities to 18 km/sec

By Charles G. Miller

View Performance analysis of Advanced Spacecraft TPS By William C. Pitts

Performance analysis of Advanced Spacecraft TPS

Performance analysis of Advanced Spacecraft TPS

By William C. Pitts

View Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids By Guruaja R. Vemaganti

Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids

Laminar and turbulent flow computations of type IV shock-shock interference aerothermal loads using unstructured grids

By Guruaja R. Vemaganti

View On ablation for the recovery of satellites By Steven Georgiev

On ablation for the recovery of satellites

On ablation for the recovery of satellites

By Steven Georgiev

View Aerothermodynamics for space vehicles By European Symposium on Aerothermodynamics for Space Vehicles (1st 1991 Noordwijk, Netherlands)

Aerothermodynamics for space vehicles

Aerothermodynamics for space vehicles

By European Symposium on Aerothermodynamics for Space Vehicles (1st 1991 Noordwijk, Netherlands)

View Planetary entry experiments By Roger Craig

Planetary entry experiments

Planetary entry experiments

By Roger Craig

View Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions By William A. Wood

Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions

Aerothermodynamic calculations on X-34 at Mach 6 wind tunnel conditions

By William A. Wood

View Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel By S. Venkateswaran

Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel

Computational method to predict thermodynamic, transport, and flow properties for the modified Langley 8-foot high-temperature tunnel

By S. Venkateswaran