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Experimental Study Of Supersonic Flow In The Prandtl Nozzle
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Book Synopsis Experimental Study of Supersonic Flow in the Prandtl Nozzle by : J. W. Dolan
Download or read book Experimental Study of Supersonic Flow in the Prandtl Nozzle written by J. W. Dolan and published by . This book was released on 1944 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Analysis of Supersonic Flow Phenomena in Conical Nozzles by a Method of Characteristics by : Linwood B. Callis
Download or read book An Analysis of Supersonic Flow Phenomena in Conical Nozzles by a Method of Characteristics written by Linwood B. Callis and published by . This book was released on 1966 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Modification of a Three-dimensional Supersonic Nozzle Analysis and Comparison with Experimental Data by : Allan R. Bishop
Download or read book Modification of a Three-dimensional Supersonic Nozzle Analysis and Comparison with Experimental Data written by Allan R. Bishop and published by . This book was released on 1974 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A computer program previously developed to analyze three-dimensional supersonic nozzles by the method of characteristics has been modified to study less restrictive nozzle geometries and nonuniform inlet conditions. An example indicates that a one-dimensional calculation that uses an averaged initial profile may be significantly in error. A comparison between the analysis and the data from a three-dimensional experiment shows generally good agreement between the two.
Book Synopsis Experimental study of an underexpanded supersonic nozzle exhausting into an expansive launch tube by : Robert Randall Morris
Download or read book Experimental study of an underexpanded supersonic nozzle exhausting into an expansive launch tube written by Robert Randall Morris and published by . This book was released on 1976 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of Supersonic Jets in Ducts by : Charles Earl Hallum
Download or read book An Experimental Study of Supersonic Jets in Ducts written by Charles Earl Hallum and published by . This book was released on 1954 with total page 178 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of Highly Cooled Boundary Layer Transition and Heat Transfer in Supersonic Flow by : Hudson Lee Conley
Download or read book An Experimental Study of Highly Cooled Boundary Layer Transition and Heat Transfer in Supersonic Flow written by Hudson Lee Conley and published by . This book was released on 1971 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Mixing of Jets and Turbulent Boundary Layers by : Harry Edward Bailey
Download or read book Supersonic Mixing of Jets and Turbulent Boundary Layers written by Harry Edward Bailey and published by . This book was released on 1958 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of the Effect of Inlet Geometry on Flow and Performance of Supersonic Nozzle by : Gerald M. Mulenberg (1LT, USAF.)
Download or read book An Experimental Study of the Effect of Inlet Geometry on Flow and Performance of Supersonic Nozzle written by Gerald M. Mulenberg (1LT, USAF.) and published by . This book was released on 1969 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Research on Transonic and Supersonic Flow of a Real Fluid at Abrupt Increases in Cross Section (with Special Consideration of Base Drag Problems) by : Helmut Hans Korst
Download or read book Research on Transonic and Supersonic Flow of a Real Fluid at Abrupt Increases in Cross Section (with Special Consideration of Base Drag Problems) written by Helmut Hans Korst and published by . This book was released on 1964 with total page 318 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Pressure-distribution Investigation of a Supersonic-aircraft Fuselage and Calibration of the Mach Number 1.40 Nozzle of the Langley 4- by 4-foot Supersonic Tunnel by : Lowell E. Hasel
Download or read book A Pressure-distribution Investigation of a Supersonic-aircraft Fuselage and Calibration of the Mach Number 1.40 Nozzle of the Langley 4- by 4-foot Supersonic Tunnel written by Lowell E. Hasel and published by . This book was released on 1950 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Study of the Influence of the Boundary Layer Thickness on the Cavity Response in a Supersonic Flow by : Gregoire Boulard
Download or read book Experimental Study of the Influence of the Boundary Layer Thickness on the Cavity Response in a Supersonic Flow written by Gregoire Boulard and published by . This book was released on 2010 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Study of Slot Injection Into a Supersonic Stream by : Michael Kenworthy
Download or read book An Experimental Study of Slot Injection Into a Supersonic Stream written by Michael Kenworthy and published by . This book was released on 1973 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of two-dimensional tangential-slot injection into a turbulent boundary layer at a freestream Mach number of 2.4 has been conducted. Nearly adiabatic surface temperatures were maintained during all tests. Static and pitot pressure profiles at four stations downstream of the slot were obtained. Skin friction was measured at the last three stations with a self-nulling balance. Schlieren photographs of the flow field were also obtained. Most of the data were obtained with slot Mach numbers of 0.31 and 0.66 corresponding to slot pressure less than and equal to stream static pressure, respectively. For the latter matched-pressure case, tangential slot injection reduced the surface shear at the three measuring stations by about 60 to 20 percent for increasing downstream distances from the slot of 12 to 28 slot heights. However, for the other case where slot pressure was less than stream static pressure, the effect of injection was to increase the shear by about 90 percent at the last downstream station of 28 slot heights. This increase in shear is attributed to the rapid acceleration of the low speed injectant stream by the high speed main stream and the increasing pressure through the recompression zone which is absent for the matched pressure case.
Book Synopsis Experimental Study of Supersonic Viscous Leeside Flow Over a Slender Delta Wing by :
Download or read book Experimental Study of Supersonic Viscous Leeside Flow Over a Slender Delta Wing written by and published by . This book was released on 1980 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of Separated Turbulent Supersonic Flow at M by : Robert Earl Wilson
Download or read book An Experimental Investigation of Separated Turbulent Supersonic Flow at M written by Robert Earl Wilson and published by . This book was released on 1966 with total page 110 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of Normal, Sonic Injection Through a Wedge-shaped Nozzle Into Supersonic Flow by : Matthew James Barber
Download or read book Experimental Investigation of Normal, Sonic Injection Through a Wedge-shaped Nozzle Into Supersonic Flow written by Matthew James Barber and published by . This book was released on 1991 with total page 392 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Computation of Supersonic Flow over Flying Configurations by : Adriana Nastase
Download or read book Computation of Supersonic Flow over Flying Configurations written by Adriana Nastase and published by Elsevier. This book was released on 2010-07-07 with total page 425 pages. Available in PDF, EPUB and Kindle. Book excerpt: Computation of Supersonic Flow over Flying Configurations is a high-level aerospace reference book that will be useful for undergraduate and graduate students of engineering, applied mathematics and physics. The author provides solutions for three-dimensional compressible Navier-Stokes layer subsonic and supersonic flows. Computational work and experimental results show the real-world application of computational results Easy computation and visualization of inviscid and viscous aerodynamic characteristics of flying configurations Includes a fully optimized and integrated design for a proposed supersonic transport aircraft
Book Synopsis An Experimental Investigation of Supersonic Flow in Long Channels by : Malcom Green
Download or read book An Experimental Investigation of Supersonic Flow in Long Channels written by Malcom Green and published by . This book was released on 1951 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: