A theoretical model for the sharp flat plate in rarefied hypersonic flow.
Rarefied hypersonic flow model for sharp flat plate in strong interaction regimes, discussing inviscid and viscous shock and merged layers subregimes
Bush, W. B.↗
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Kinetic theory of the sharp leading edge problem. I - Supersonic flow.
Kinetic theory of sharp leading edge parallel to supersonic flow using Boltzmann equation, determining flow field
Hartley, D. L.↗
Kinetic theory of the sharp leading edge problem in supersonic flow.
Boltzmann equation with BGK model as governing equation for sharp leading edge problem in supersonic flow
Hartley, D. L.↗
Vortex breakdown on slender sharp-edged wings.
Vortex breakdown on slender sharp edged and modified delta wings with varying sweep angles investigated in wind tunnel using schlieren system for flow visualization
Kohlman, D. L.↗
The Sharps chondrite - New evidence on the origin of chondrules and chondrites.
Sharps chondrite chemical, petrographic and mineralogical studies suggesting formation from complex and repetitious high temperature events and agglomeration processes
Fredriksson, K.↗
Hypersonic viscous interaction on sharp and blunt inclined plates.
Mach 42 test measuring surface pressures, surface heat transfer rates and shock wave shapes in strong interaction regime for sharp and blunt plates
Kemp, J. H., Jr.↗
On the sharpness of cracks compared with Wells' COD
Sharpness of cracks compared with Wells crack opening displacements
Roberts, E., Jr.↗
Laminar Reynolds analogy factor on a sharp flat plate at Mach 10.4
Values measured on sharp flat plate in 10.4 Mach boundary layer induced pressure gradient, discussing effects of wall pressure and temperature gradients
Stone, H. W.↗
Surface pressures and shock-wave shapes on sharp plates and wedges in low-density hypersonic flow
Surface pressures and shock wave shapes on sharp flat plates and wedges in rarefied hypersonic transition flow with emphasis on merged layer regime
Horstman, C. C.↗
An experimental study of hypersonic rarefied flow over sharp cones
Hypersonic rarefied merged layer flow over sharp slender cones, using strong interaction theory and free molecular flow to analyze surface pressures
Horstman, C. C.↗
A time-dependent method for calculating supersonic blunt-body flow fields with sharp corners and embedded shock waves
Time-dependant method for calculating supersonic blunt body flow fields with sharp corners and embedded shock waves
Barnwell, R. W.↗
Flow fields over sharp edged delta wings with attached shocks
Analysis of supersonic and hypersonic flow of inviscid ideal gas over conical wings with sharp leading edges and attached shock waves by three dimensional method of characteristics
Beeman, E. R., Jr.↗
Comparison of wind tunnel and flight-measured base pressures from the sharp-leading-edge upper vertical fin of the X-15 airplane for turbulent flow at Mach numbers from 1.5 to 5.0
Flight-measured base pressures from sharp leading edge upper vertical fin of X-15 aircraft compared with wind tunnel data for turbulent flow at Mach numbers from 1.5 to 5.0
Goecke, S. A.↗
Experimental and analytical investigation of subsonic longitudinal and lateral aerodynamic characteristics of slender sharp edge 74 deg swept wings
Experimental and analytical study of subsonic longitudinal and lateral aerodynamic characteristics of slender sharp edge 74 deg swept wings
Davenport, E. E.↗
Computer program for design of two-dimensional sharp-edged-throat supersonic nozzle with boundary layer correction
FORTRAN 4 computer program for design of sharp-edged-throat supersonic nozzles with boundary layer correction
Goldman, L. J.↗
Three-dimensional flow around blunt bodies with sharp shoulders
Three dimensional inviscid compressible flow past sharp shouldered blunt bodies at angle of attack, presenting time dependent finite difference technique
Barnwell, R. W.↗
Vortex breakdown on slender sharp-edged wings
Vortex breakdown on slender sharp edged and modified delta wings with varying sweep angles investigated in wind tunnel using schlieren system for flow visualization
Kohlman, D. L.↗
Sharp slender cones in near-free-molecule hypersonic flow
Shock tunnel drag measurements on sharp slender cones in near free molecule hypersonic flow in air and He
Horstman, C. C.↗