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.↗
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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.↗
Calculated and experimental hinge moments on a trailing-edge flap of a 75 deg swept delta wing at Mach 6
Calculated and experimental hinge moments on trailing-edge flaps of swept delta wings at hypersonic speeds and positive deflection angles
Ashby, G. C., Jr.↗
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.↗
Sensitivity of the creep-rupture properties of nickel-base superalloy sheet to sharp edge-notches in the temperature range of 1000 deg F - 1400 deg F
Edge notch sensitivity in thin sheet nickel alloys under stress at high temperatures
Freeman, J. W.↗
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.↗
The leading edge effects on a laminar flat- plate boundary layer at Mach 10.4
Leading edge effects on laminar flat-plate boundary layer at Mach 10.4
Stone, H. W.↗
The leading-edge effects on the laminar flat- plate boundary layer and the aerodynamic heating at Mach 10.4
Leading edge effects on laminar flat plate boundary layer and aerodynamic heating at Mach 10.4
Stone, H. W.↗
Pressures and heat transfer on a 75 degree swept delta wing with trailing-edge flap at Mach 6 and angles of attack to 90 degrees
Pressure and heat transfer on swept delta wing with trailing-edge flap
Keyes, J. W.↗
Development of three-dimensional pressure- distribution functions for lifting surfaces with trailing-edge controls based on the integral equation for subsonic flow
Three dimensional pressure distribution functions for lifting surfaces with trailing-edge controls based on integral equations for subsonic flow
Crespo, A. N.↗
Flight test results of a trailing edge flap designed for direct-lift control
Boundary layer control and trailing edge flaps for direct-lift control
Taylor, C. R., Jr.↗
Cold air investigation of a turbine with stator-blade trailing-edge coolant ejection. Part 1 - Overall stator performance
Stator performance with cooling by air ejection from trailing edges of blades
Behning, F. P.↗
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.↗
Experimental investigation of the cooling and structural performance for the HRE cowl leading edge
Cooling and structural performance of hypersonic research engine cowl leading edge
Jilly, L. F.↗
Flow phenomena and separation over delta wings with trailing-edge flaps at Mach 6.
Hypersonic flow distribution and separation types over highly swept delta wings with trailing edge flaps at Mach 6
Keyes, J. W.↗
Elastic displacements for various edge-cracked plate specimens.
Elastic displacements for edge cracked plate specimens used as crack extension indicator in plane strain fracture toughness measurements
Gross, 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.↗
Elastic crack-edge displacements for the compact tension specimen.
Displacements and stress intensity as function of crack length for compact tension specimen, considering load line and crack edge
Roberts, E., Jr.↗