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Author : Stephen W. D. Wolf
Publisher :
ISBN 13 :
Total Pages : 88 pages
Book Rating : 4.:/5 (31 download)
Download or read book Supersonic Wind Tunnel Nozzles written by Stephen W. D. Wolf and published by . This book was released on 1990 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Ralph C. Tolle
Publisher :
ISBN 13 :
Total Pages : 274 pages
Book Rating : 4.3/5 (91 download)
Download or read book Development and Testing of a New Optimum Design Code for Hypersonic Wind Tunnel Nozzles, Including Boundary Layer, Turbulence, and Real Gas Effects written by Ralph C. Tolle and published by . This book was released on 1996 with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722368340
Total Pages : 42 pages
Book Rating : 4.3/5 (683 download)
Download or read book Method of Characteristics Design of a Supersonic Wind Tunnel Nozzle with Square Cross-Section, Supplement 3 written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-05 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: Nozzle design codes developed earlier were modified and used in order to design a supersonic wind tunnel nozzle with square cross-sections. As part of the design process, a post-processing code that generates square nozzles from the output of the Sivells code was written. The method is based on the results of an axisymmetric method of characteristics code and an axisymmetric boundary layer code. These design codes are documented. Schneider, Steven P. Unspecified Center NAG1-1133...
Author : David Shore
Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.:/5 (621 download)
Download or read book Boundary Layers in Supersonic Wind Tunnel Nozzles written by David Shore and published by . This book was released on 1950 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : D. Pierce
Publisher :
ISBN 13 :
Total Pages : 21 pages
Book Rating : 4.:/5 (864 download)
Download or read book A Simple Flexible Supersonic Wind Tunnel Nozzle for the Rapid and Accurate Variation of Flow Mach Number written by D. Pierce and published by . This book was released on 1965 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Thomas Bernard Schaffer
Publisher :
ISBN 13 :
Total Pages : 176 pages
Book Rating : 4.E/5 ( download)
Download or read book The Design of a Variable Throat Rectangular Nozzle for a Supersonic Wind Tunnel written by Thomas Bernard Schaffer and published by . This book was released on 1947 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. Hermann
Publisher :
ISBN 13 :
Total Pages : 13 pages
Book Rating : 4.:/5 (977 download)
Download or read book Condensation shock waves in supersonic wind tunnel nozzles written by R. Hermann and published by . This book was released on with total page 13 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John B. Anders
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)
Download or read book Fluid Flow Analysis of a Hot-core Hypersonic-wind-tunnel Nozzle Concept written by John B. Anders and published by . This book was released on 1972 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A hypersonic-wind-tunnel nozzle concept which incorporates a hot-core flow surrounded by an annular flow of cold air offers a promising technique for maximizing the model size while minimizing the power required to heat the test core. This capability becomes especially important when providing the true-temperature duplication needed for hypersonic propulsion testing. Several two-dimensional wind-tunnel nozzle configurations that are designed according to this concept are analyzed by using recently developed analytical techniques for prediction of the boundary-layer growth and the mixing between the hot and cold coaxial supersonic airflows. The analyses indicate that introduction of the cold annular flow near the throat results in an unacceptable test core for the nozzle size and stagnation conditions considered because of both mixing and condensation effects. Use of a half-nozzle with a ramp on the flat portion does not appear promising because of the thick boundary layer associated with the extra length. However, the analyses indicate that if the cold annular flow is introduced at the exit of a full two-dimensional nozzle, an acceptable test core will be produced. Predictions of the mixing between the hot and cold supersonic streams for this configuration show that mixing effects from the cold flow do not appreciably penetrate into the hot core for the large downstream distances of interest.
Author : Margaret A. Davis
Publisher :
ISBN 13 :
Total Pages : 90 pages
Book Rating : 4.:/5 (151 download)
Download or read book Calibration of the Mach Number 2.9 Nozzle in the Supersonic Wind Tunnel written by Margaret A. Davis and published by . This book was released on 1952 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. W. Peterson
Publisher :
ISBN 13 :
Total Pages : 5 pages
Book Rating : 4.:/5 (977 download)
Download or read book Nozzle Design for the Supersonic Wind Tunnel written by J. W. Peterson and published by . This book was released on 1948 with total page 5 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : William F. MacInnes
Publisher :
ISBN 13 :
Total Pages : 108 pages
Book Rating : 4.:/5 (152 download)
Download or read book An Experimental Investigation of the Mach Two Nozzle, UCLA Supersonic Wind Tunnel written by William F. MacInnes and published by . This book was released on 1954 with total page 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Riordan Howard Tesling Cox
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (927 download)
Download or read book Supersonic Wind-tunnel written by Riordan Howard Tesling Cox and published by . This book was released on 1972* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : James Conlan
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (227 download)
Download or read book A High Speed Computer Technique to Determine Nozzle Contours for Supersonic Wind Tunnels written by James Conlan and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report describes a computer program developed at the Naval Ordnance Laboratory to calculate contours for supersonic wind tunnel nozzles. Both two-dimensional and axi-symmetric flow is covered and the technique arises from the method of characteristics in the theory of solution of hyperbolic partial differential equations. (Author).
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
ISBN 13 : 9781722791766
Total Pages : 60 pages
Book Rating : 4.7/5 (917 download)
Download or read book Effect of Heating and Cooling Strips on Boundary Layer Stability of Nozzles and Test Sections of Supersonic Wind Tunnels written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-16 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The objective of the research is to understand supersonic laminar flow stability, transition, and active control. Some prediction techniques will be developed or modified to analyze laminar flow stability. The effects of supersonic laminar flow with distributed heating and cooling on active control will be studied. The primary tasks of the research applying to the NASA/Ames Proof of Concept (POC) Supersonic Wind Tunnel and Laminar Flow Supersonic Wind Tunnel (LFSWT) nozzle design with laminar flow control are as follows: (1) predictions of supersonic laminar boundary layer stability and transition, (2) effects of wall heating and cooling for supersonic laminar flow control, and (3) performance evaluation of POC and LFSWT nozzles design with wall heating and cooling effects applying at different locations and various length. Lo, Ching F. Unspecified Center...
Author :
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (141 download)
Download or read book A Summary of the Techniques of Variable Mach Number Supersonic Wind Tunnel Nozzle Design written by and published by . This book was released on 1954 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Amir Houshang Tajfar
Publisher :
ISBN 13 :
Total Pages : 99 pages
Book Rating : 4.:/5 (15 download)
Download or read book Nozzle Design for Supersonic and Hypersonic Wind Tunnels written by Amir Houshang Tajfar and published by . This book was released on 1990 with total page 99 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)
Download or read book The High-speed Flexible-throat Supersonic Wind Tunnel written by and published by . This book was released on 1948 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
