Pressure probes for fluid measurement
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[1] F. A. Macmillan,et al. Viscous Effects on Pitot Tubes at Low Speeds , 1954, The Journal of the Royal Aeronautical Society.
[2] John R Erwin,et al. Several Combination Probes for Surveying Static and Total Pressure and Flow Direction , 1952 .
[3] George M Low,et al. Factors affecting laminar boundary layer measurements in a supersonic steam , 1953 .
[4] H. Pond,et al. The Effect of Entrance Velocity on the Flow of a Rarefied Gas Through a Tube , 1962 .
[5] J. H. Chang,et al. VISCOUS EFFECTS ON IMPACT PRESSURE MEASUREMENTS IN LOW DENSITY FLOWS AT HIGH MACH NUMBERS , 1968 .
[6] Kenneth G Merriam,et al. Comparative tests of Pitot-static tubes , 1935 .
[7] M. J. Lighthill,et al. Contributions to the theory of the Pitot-tube displacement effect , 1957, Journal of Fluid Mechanics.
[8] N. H. Kemp,et al. VISCOUS AERODYNAMIC CHARACTERISTICS IN HYPERSONIC RAREFIED GAS FLOW. Research Report 48 (Revised) , 1959 .
[9] P. Clausing,et al. Über die Strömung sehr verdünnter Gase durch Röhren von beliebiger Länge , 1932 .
[10] J. F. Hahn. The Effect of Mach Number, Incidence and Hole Position on the Static Pressure Measured by a Square Ended Probe , 1964, The Journal of the Royal Aeronautical Society.
[11] I. Amdur,et al. Kinetic Theory of Gases , 1959 .
[12] William Gracey,et al. Wind-tunnel investigation of a shielded total-pressure tube at transonic speeds , 1952 .
[13] C Frederick Hansen,et al. Condensation of air in supersonic wind tunnels and its effects on flow about models , 1952 .
[14] M. Glauert,et al. The method of images in shear flow , 1960, Journal of Fluid Mechanics.
[15] Robert M O'Donnell. Experimental Investigation at a Mach Number of 2.41 of Average Skin-friction Coefficients and Velocity Profiles for Laminar and Turbulent Boundary Layers and an Assessment of Probe Effects , 1954 .
[16] J. L. Livesey,et al. The Static Hole Error Problem , 1962 .
[17] W. S. Bradfield. The Effect of Leading-Edge Bluntness on a Laminar Supersonic Boundary Layer , 1954 .
[18] P. O. A. L. Davies,et al. The behaviour of a Pitot tube in transverse shear , 1958, Journal of Fluid Mechanics.
[19] M. R. Head,et al. The Preston tube as a means of measuring skin friction , 1962, Journal of Fluid Mechanics.
[20] A. B. Bailey,et al. Pressures in the stagnation regions of blunt bodies in rarefied flow , 1964 .
[21] E. S. Levinsky,et al. RAREFIED HYPERSONIC FLOW OVER A SPHERE. , 1962 .
[22] A. M. Tyndall,et al. XLII. On the value of the pitot constant , 1911 .
[23] Ann Arbor,et al. Review of the Pitot tube , 1956 .
[24] Otto Conrad. Geräte zur Messung von Strömungsrichtungen , 1950 .
[25] W. Aichelen. Der geometrische Ort für die mittlere Geschwindigkeit bei turbulenter Strömung in glatten und rauhen Rohren , 1947 .
[26] Alan Quarmby,et al. Displacement Effects on Pitot Tubes with Rectangular Mouths , 1969 .
[27] J. M. Marchello,et al. Impact tube size in fluid velocity measurement , 1964 .
[28] Jules L. Dussourd,et al. A Deceleration Probe for Measuring Stagnation Pressure and Velocity of a Particle-Laden Gas Stream , 1958 .
[29] D. Surry,et al. Two Probes for the Measurement of the Complete Velocity Vector in Subsonic Flow , 1968 .
[30] F Homann. The effect of high viscosity on the flow around a cylinder and around a sphere , 1952 .
[31] F. S. Sherman,et al. The Structure and Utilization of Supersonic Free Jets in Low Density Wind Tunnels , 1965 .
[32] F A Louden,et al. Tables for pressure of air on coming to rest from various speeds , 1927 .
[33] J. H. Whitelaw,et al. Simplification of the Razor Blade Technique and its Application to the Measurement of Wall-Shear Stress in Wall-Jet Flows , 1969 .
[34] M. J. Lighthill,et al. The fundamental solution for small steady three-dimensional disturbances to a two-dimensional parallel shear flow , 1957, Journal of Fluid Mechanics.
[35] Paul E Hemke. Influence of the Orifice on Measured Pressures , 1926 .
[36] J. H. D. Leeuw,et al. THE FREE-MOLECULE IMPACT-PRESSURE PROBE OF ARBITRARY LENGTH , 1963 .
[37] A. Bailey,et al. PRESSURES IN THE STAGNATION REGIONS OF BLUNT BODIES IN THE VISCOUS-LAYER TO MERGED-LAYER REGIMES OF RAREFIED FLOW , 1963 .
[38] N. Rajaratnam. A Note on the Static Hole Error Problem , 1966, The Journal of the Royal Aeronautical Society.
[39] Roy E Rayle,et al. An investigation of the influence of orifice geometry on static pressure measurements , 1949 .
[40] S. A. Schaaf,et al. The Theory of the Impact Tube at Low Pressures , 1948 .
[41] F. V. Davies. Some effects of pitot size on the measurement of boundary layers in supersonic flow , 1952 .
[42] D. E. Boylan,et al. An Influence of the Orifice on Measured Pressures in Rarefied Flow , 1965 .
[43] R. J. Monaghan. The use of pitot tubes in the measurement of laminar boundary layers in supersonic flow , 1955 .
[44] A. H. Glaser. The Pitot cylinder as a static pressure probe in turbulent flow , 1952 .
[45] Arthur Kantrowitz,et al. Heat‐Capacity Lag in Gas Dynamics , 1946 .
[46] Jack C. Graves. Impact pressure and total temperature interpretation at hypersonic mach number. , 1954 .
[47] S. A. Schaaf,et al. Effect of slip on flow near a stagnation point and in a boundary layer , 1951 .
[48] Geoffrey Ingram Taylor,et al. The Air Pressure on a Cone Moving at High Speeds. II , 1933 .
[49] R. C. Pankhurst,et al. The Measurement of Air Flow , 1928, Nature.
[50] Dorothy Marshall,et al. On the Conditions at the Boundary of a Fluid in Turbulent Motion , 1920 .
[51] R. Shaw,et al. The influence of hole dimensions on static pressure measurements , 1960, Journal of Fluid Mechanics.
[52] A. Kumar Ray,et al. Einfluß der Bohrlochgröße auf die Anzeige des statischen Druckes bei verschiedenen Reynoldszahlen , 1956 .
[53] M. R. Head,et al. Some observations on skin friction and velocity profiles in fully developed pipe and channel flows , 1969, Journal of Fluid Mechanics.
[54] J. H. Preston. The Determination of Turbulent Skin Friction by Means of Pitot Tubes , 1954, The Journal of the Royal Aeronautical Society.
[55] H. K. Das,et al. Measurement of Skin Friction using a Rectangular Mouthed Preston Tube , 1969 .
[56] J. L. Livesey. The Behavior of Transverse Cylindrical and Forward Facing Total Pressure Probes in Transverse Total Pressure Gradients , 1956 .
[57] I. M. Hall. The displacement effect of a sphere in a two-dimensional shear flow , 1956, Journal of Fluid Mechanics.
[58] F. A. Macmillan. Viscous Effects on Flattened Pitot Tubes at Low Speeds , 1954, The Journal of the Royal Aeronautical Society.
[59] H. Rouse,et al. Cavitation and pressure distribution: head forms at zero angle of yaw , 1948 .
[60] Morton Cooper,et al. The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds , 1951 .
[61] M. R. Head,et al. Simplified Presentation of Preston Tube Calibration , 1971 .
[62] V. C. Patel. Calibration of the Preston tube and limitations on its use in pressure gradients , 1965, Journal of Fluid Mechanics.
[63] N. Rajaratnam,et al. Yaw Probe used as Preston Tube , 1968, The Aeronautical Journal (1968).
[64] Alan Quarmby,et al. An experimental study of turbulent flow through concentric annuli , 1967 .
[65] D. J. Richardson,et al. A SHORT STATIC PROBE WITH GOOD INCIDENCE CHARACTERISTICS AT SUPERSONIC SPEED , 1967 .
[66] Alan Quarmby. On the Use of the Preston Tube in Concentric Annuli , 1967, The Journal of the Royal Aeronautical Society.
[67] J. L. Livesey. Design of Total Pressure Probes for Minimum Interference with Measured Flow , 1954 .