Observations of the lunar Mach cone
Confirming existance of lunar Mach cones by magnetometer data from Explorer 35
Ness, N. F.↗
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Results for “CONES”
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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Shock wave shapes and surface pressures on hemisphere and cone cylinders in low density hypersonic flow including ablation
Shock-wave shapes and surface pressures on hemisphere and cone cylinders in low density hypersonic flow including ablation
Kuehn, D. M.↗
Flow-field investigation for large-angle cones with short spikes at a Mach number of 9.6
Flow distribution for large angle cones with short spikes in hypersonic laminar flow
Staylor, W. F.↗
An experimental investigation of boundary- layer transition on a 10 deg half-angle cone at Mach 6.9
Boundary layer transition on nose cones at hypersonic speeds
Fischer, M. C.↗
Inviscid hypersonic flow of chemically relaxing air about pointed circular cones
Inviscid hypersonic flow of chemically relaxing air about pointed circular cones
Thoenes, J.↗
Aerodynamic interference effects on half-cone bodies with thin wings at Mach 10.03
Aerodynamic interference effects on half-cone bodies with thin wings in hypersonic flow
Townsend, J. C.↗
Effects of angle of attack and bluntness on the hypersonic flow over a 15 deg semiapex cone in helium
Angle of attack and bluntness effects on hypersonic flow over 15 deg semiapex cone in helium
Cleary, J. W.↗
A method for predicting pressures on elliptic cones at supersonic speeds
Two dimensional shock theory for predicting pressures on elliptic cones at supersonic speeds
Kaattari, G. E.↗
Detailed pressure distribution on a blunted 60-deg half-angle cone at Mach numbers of 6.08 and 9.46
Pressure distribution of spherically-blunted 60 deg half-angle cone in hypersonic flow
Kurtz, D. W.↗
Study of convective heat transfer to cones and cylinders at angle of attack Final report
Convective heat transfer to cones and cylinders at angle of attack
Bhadsavle, A. G.↗
Angle-of-attack analysis of a spinning slender cone with slight aerodynamic and mass asymmetries /reentry F/
Angle of attack analysis of spinning slender reentry cone with slight aerodynamic and mass asymmetries
Morris, W. D.↗
Free-flight measurements of dynamic stability derivatives of a blunted 120 deg cone in helium at Mach number 15.4
Free flight measurements of dynamic stability derivatives of blunted 120 deg cone in helium compared to unmodified Newtonian theory predictions
Carter, J. E.↗
Hypersonic boundary-layer transition on ablating and nonablating cones
Ablation effects on transition Reynolds number of hypersonic boundary layer on slender cones
Fischer, M. 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.↗
Correction for the ordinary Mangler displacement thickness for slender cones
Mangler displacement thickness correction for slender cones
Bradley, R. H.↗
Cone drag in rarefied hypersonic flow
Drag coefficients for spheres and sharp cones in rarefied hypersonic air flow obtained in shock tunnel using free flight technique
Horstman, C. C.↗
Ballistic range tests of ablating and nonablating slender cones
Ballistic range tests to study ablation effects on aerodynamic characteristics of ablating and nonablating slender cones
Chapman, G. T.↗
Comparison of free-flight experimental results with theory on the nonlinear aerodynamic effects of bluntness for slender cones at Mach number 17
Aerodynamic effects of bluntness on slender cones in free flight tests at Mach 17
Malcolm, G. N.↗