Computer program for design of two dimensional supersonic nozzle with sharp edged throat
FORTRAN 4 program for computerized design of two dimensional supersonic nozzles with sharp edged throats
Goldman, L. J.↗
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Results for “SHARP”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Application of the leading-edge-suction analogy of vortex lift to the drag due to lift of sharp-edge delta wings
Sharp edge delta wing drag prediction by application of leading edge suction analogy of vortex lift
Polhamus, E. C.↗
Boundary-layer transition on sharp cones at hypersonic Mach numbers.
Transition from laminar to turbulent boundary layer flow on sharp cones hypersonic Mach numbers, noting measurement techniques
Henderson, A., Jr.↗
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.↗
Stress-birefringent patterns of a viscoelastic fluid at a sharp-edged entrance.
Stress-birefringent patterns of viscoelastic fluid flowing into sharp edged channel entrance, discussing shear stresses
Bogue, D. C.↗
Kinetic theory of the sharp leading edge problem. II - Hypersonic flow.
Hypersonic sharp leading edge problem, determining density, temperature, velocity and surface pressure profiles with kinetic theory of gases
Huang, A. B.↗
Wind tunnel investigations of vortex breakdown on slender sharp edged wings Final report
Wind tunnel tests of vortex breakdown on sharp edged delta wings
Kohlman, D. L.↗
Prediction of lift and drag for slender sharp-edge delta wings in ground proximity
Predicting lift and drag for slender sharp-edge Delta wings in ground proximity
Fox, C. H., Jr.↗
Aerodynamic investigation of sharp cone- cylinder spikes on 120 degree blunted cones at Mach numbers of 3.00, 4.50, and 6.00
Aerodynamic investigation of sharp cone-cylinder spikes on 120 degree blunted cones at Mach numbers of 3, 4.5, and 6
Mc Ghee, R. J.↗
An analytical method for predicting the lift and drag for slender sharp-edge delta wings in ground proximity
Analytical method for predicting lift and drag for slender sharp-edge delta wings near ground level
Fox, C. H., Jr.↗
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.↗
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.↗