Author : Anonim
Publisher : Unknown
Page : 586 pages
File Size : 48,7 Mb
Release : 1976
Category : Electronic
ISBN : MINN:31951000846582R
Effect Of Blockage Ratio On Drag And Pressure Distributions For Bodies Of Revolution At Transonic Speeds
Effect Of Blockage Ratio On Drag And Pressure Distributions For Bodies Of Revolution At Transonic Speeds Book in PDF, ePub and Kindle version is available to download in english. Read online anytime anywhere directly from your device. Click on the download button below to get a free pdf file of Effect Of Blockage Ratio On Drag And Pressure Distributions For Bodies Of Revolution At Transonic Speeds book. This book definitely worth reading, it is an incredibly well-written.
Effect of Blockage Ratio on Drag and Pressure Distributions for Bodies of Revolution at Transonic Speeds
Author : Lana M. Couch,Cuyler W. Brooks (Jr.)
Publisher : Unknown
Page : 116 pages
File Size : 43,5 Mb
Release : 1973
Category : Aerodynamic load
ISBN : UIUC:30112106885517
Effect of Blockage Ratio on Drag and Pressure Distributions for Bodies of Revolution at Transonic Speeds by Lana M. Couch,Cuyler W. Brooks (Jr.) Pdf
Experimental data were obtained in two wind tunnels for 13 models over a Mach number range from 0.70 to 1.02. Effects of increasing test-section blockage ratio in the transonic region near a Mach number of 1.0 included change in the shape of the drag curves, premature drag creep, delayed drag divergence, and a positive increment of pressures on the model afterbodies. Effects of wall interference were apparent in the data even for a change in blockage ratio from a very low 0.000343 to an even lower 0.000170. Therefore, models having values of blockage ratio of 0.0003 - an order of magnitude below the previously considered safe value of 0.0050 - had significant errors in the drag-coefficient values obtained at speeds near a Mach number of 1.0. Furthermore, the flow relief afforded by slots or perforations in test-section walls - designed according to previously accepted criteria for interference-free subsonic flow - does not appear to be sufficient to avoid significant interference of the walls with the model flow field for Mach numbers very close to 1.0.
Monthly Catalog of United States Government Publications
Author : Anonim
Publisher : Unknown
Page : 1570 pages
File Size : 47,9 Mb
Release : 1974
Category : Government publications
ISBN : STANFORD:36105006329010
Monthly Catalog of United States Government Publications by Anonim Pdf
Monthly Catalog of United States Government Publications, Cumulative Index
Author : United States. Superintendent of Documents
Publisher : Unknown
Page : 1408 pages
File Size : 44,5 Mb
Release : 1976
Category : United States
ISBN : STANFORD:36105021034173
Monthly Catalog of United States Government Publications, Cumulative Index by United States. Superintendent of Documents Pdf
NASA Technical Memorandum
Author : Anonim
Publisher : Unknown
Page : 224 pages
File Size : 45,5 Mb
Release : 1980
Category : Aeronautics
ISBN : MINN:31951000845212T
NASA Technical Memorandum by Anonim Pdf
Asymptotic and Numerical Methods for Partial Differential Equations with Critical Parameters
Author : H.G. Kaper,Marc Garbey
Publisher : Springer Science & Business Media
Page : 371 pages
File Size : 49,6 Mb
Release : 2012-12-06
Category : Mathematics
ISBN : 9789401118101
Asymptotic and Numerical Methods for Partial Differential Equations with Critical Parameters by H.G. Kaper,Marc Garbey Pdf
This volume contains the proceedings of the NATO Advanced Research Workshop on "Asymptotic-induced Numerical Methods for Partial Differ ential Equations, Critical Parameters, and Domain Decomposition," held at Beaune (France), May 25-28, 1992. The purpose of the workshop was to stimulate the integration of asymp totic analysis, domain decomposition methods, and symbolic manipulation tools for the numerical solution of partial differential equations (PDEs) with critical parameters. A workshop on the same topic was held at Argonne Na tional Laboratory in February 1990. (The proceedings were published under the title Asymptotic Analysis and the Numerical Solu.tion of Partial Differ ential Equations, Hans G. Kaper and Marc Garbey, eds., Lecture Notes in Pure and Applied Mathematics. Vol. 130, ·Marcel Dekker, Inc., New York, 1991.) In a sense, the present proceedings represent a progress report on the topic area. Comparing the two sets of proceedings, we see an increase in the quantity as well as the quality of the contributions. 110re research is being done in the topic area, and the interest covers serious, nontrivial problems. We are pleased with this outcome and expect to see even more advances in the next few years as the field progresses.
Transonic Aerodynamics
Author : L. Pamela Cook
Publisher : SIAM
Page : 98 pages
File Size : 42,8 Mb
Release : 1993-01-01
Category : Technology & Engineering
ISBN : 9780898713107
Transonic Aerodynamics by L. Pamela Cook Pdf
This volume offers exciting results, perspectives, and case studies for the treatment of problems arising in transonic aerodynamics. New advances including triple deck theory, analysis of stagnation at the nose of a body, transonic choked flow, and the transonic area rule are presented. Interest in analyzing the transonic range of flight, its stability properties, and especially the question of designing reduced drag (shockless or weak shock) airfoils keeps growing. Present day commercial aircraft cruise in the transonic range. Mechanical and aeronautical engineers interested in compressible fluid flows, design of optimal wings, and an understanding of transonic flow held about wings and airfoils will find the book invaluable. This book is understandable to those with a knowledge of continuum mechanics (fluids) and asymptotic methods. It is appropriate for graduate courses in aerodynamics and mathematical methods.
The High-speed Frontier
Author : John Vernon Becker
Publisher : Unknown
Page : 204 pages
File Size : 53,8 Mb
Release : 1980
Category : Government publications
ISBN : UIUC:30112047353427
The High-speed Frontier by John Vernon Becker Pdf
The High-speed Frontier. Case Histories of Four NACA Programs, 1920 - 1950
Author : John V Becker
Publisher : Unknown
Page : 204 pages
File Size : 55,6 Mb
Release : 1980
Category : Aerodynamics
ISBN : NASA:31769000420300
The High-speed Frontier. Case Histories of Four NACA Programs, 1920 - 1950 by John V Becker Pdf
An Investigation of Three-dimensional Wall Interference in a Variable Porosity Transonice Wind Tunnel
Author : Travis W. Binion (Jr.)
Publisher : Unknown
Page : 88 pages
File Size : 42,9 Mb
Release : 1974
Category : Mach number
ISBN : UOM:39015104958627
An Investigation of Three-dimensional Wall Interference in a Variable Porosity Transonice Wind Tunnel by Travis W. Binion (Jr.) Pdf
NASA Technical Report
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Page : 936 pages
File Size : 48,6 Mb
Release : 1973
Category : Aerodynamics
ISBN : UOM:39015039957116
NASA Technical Report by United States. National Aeronautics and Space Administration Pdf
NASA Reference Publication
Author : Anonim
Publisher : Unknown
Page : 76 pages
File Size : 46,9 Mb
Release : 1979
Category : Astronautics
ISBN : OSU:32435063101117
NASA Reference Publication by Anonim Pdf
Applied Mechanics Reviews
Author : Anonim
Publisher : Unknown
Page : 628 pages
File Size : 49,9 Mb
Release : 1974
Category : Mechanics, Applied
ISBN : UCAL:C2682445
Applied Mechanics Reviews by Anonim Pdf
Static and Magnus Aerodynamic Characteristics of the 155mm, M483 Projectile and Its Modifications
Author : R. W. Kline,T. D. Hoffman
Publisher : Unknown
Page : 556 pages
File Size : 53,8 Mb
Release : 1976
Category : Aerodynamics, Transonic
ISBN : UOM:39015095299478
Static and Magnus Aerodynamic Characteristics of the 155mm, M483 Projectile and Its Modifications by R. W. Kline,T. D. Hoffman Pdf
Wind Tunnel Investigation of Three Axisymmetric Cowls of Different Lengths at Mach Numbers from 0.60 to 0.92
Author : Richard J. Re
Publisher : Unknown
Page : 292 pages
File Size : 45,6 Mb
Release : 1993
Category : Airplanes
ISBN : NASA:31769000522436