Boundary-layer transition experiments on sharp, slender cones in supersonic freeflight

Reda, Daniel C.

doi:10.2514/6.1978-1129

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Cited by 9 publications

(1 citation statement)

References 27 publications

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“…Past experiments have been unable to adequately (1) control the generation of stationary crossflow waves or (2) study the growth of potential secondary instabilities. The secondary instabilities could be important to the breakdown of the stationary waves and the transition to turbulence in the boundary layer.…”

Section: Objectivesmentioning

confidence: 99%

Secondary Instabilities of Hypersonic Stationary Crossflow Waves

Edelman

2018

AIAA Journal

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Section: Objectivesmentioning

confidence: 99%

Secondary Instabilities of Hypersonic Stationary Crossflow Waves

Edelman

2018

AIAA Journal

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Flight vehicle aerodynamics calculated by a Galerkin finite element/finite difference method

Holt

Meade

1992

Computing Systems in Engineering

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Heat transfer measurement of turbulent spots in a hypersonic blunt-body boundary layer

et al. 2006

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This paper presents data on turbulent-spot propagation in the hypersonic boundarylayer flow over a blunted cylindrical body. Data are based on the measurement of time-dependent surface heat transfer rates using gauges positioned as arrays in either the axial or transverse directions. These are used to provide data on individual spots, including sectional profiles, characteristic spot planform geometries, propagation speeds, growth rates and some information on the development of an internal thermal cell structure and corresponding thermal streaks in the base or calm region of the spot.

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Boundary-layer transition experiments on sharp, slender cones in supersonic freeflight

Cited by 9 publications

References 27 publications

Secondary Instabilities of Hypersonic Stationary Crossflow Waves

Secondary Instabilities of Hypersonic Stationary Crossflow Waves

Flight vehicle aerodynamics calculated by a Galerkin finite element/finite difference method

Heat transfer measurement of turbulent spots in a hypersonic blunt-body boundary layer

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