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christopher e glass

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Shock wave interactionNumerical simulation of low-density shock-wave interactionsChristopher E. Glass

Numerical simulation of low-density shock-wave interactions

Christopher E. Glass · National Aeronautics and Space Administration, Langley Research Center

Sayfa sayısı yok · 1999

Computational fluid dynamics / Computerized simulation / Low density flow / Shock wave interaction

AerothermodynamicsAerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5Christopher E. Glass

Aerothermal tests of quilted dome models on a flat plate at a Mach number of 6.5

Christopher E. Glass · National Aeronautics and Space Administration, Scientific and Technical Information Division

Sayfa sayısı yok · 1988

Aerothermodynamics

Leading edges (Aerodynamics)Experimental study of pressure and heating rate on a swept cylindrical leading edge resulting from swept shock wave interferenceChristopher E. Glass

Experimental study of pressure and heating rate on a swept cylindrical leading edge resulting from swept shock wave interference

Christopher E. Glass · National Aeronautics and Space Administration

Sayfa sayısı yok · 1989

Interference (Aerodynamics) / Leading edges (Aerodynamics)

Computer programsComputer program to solve two-dimensional shock-wave interference problems with an equilibrium chemically reacting air modelChristopher E. Glass

Computer program to solve two-dimensional shock-wave interference problems with an equilibrium chemically reacting air model

Christopher E. Glass · For sale by the National Technical Information Service]

Sayfa sayısı yok · 1990

Hypersonic planes / Shock waves / Computer programs

Pressure distributionAerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5Christopher E. Glass

Aerothermal tests of spherical dome protuberances on a flat plate at a Mach number of 6.5

Christopher E. Glass · Langley Research Center

58 sayfa · 1986

Laminar boundary layer / Turbulent boundary layer / Thermal protection / Hypersonic aircraft / Pressure distribution