A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels

A Comparison of Transition Reynolds Numbers from 12-in. and 40-in. Supersonic Tunnels
Author: C. J. Schueler
Publisher:
Total Pages: 42
Release: 1963
Genre: Aerodynamics, Supersonic
ISBN:

Transition Reynolds number measurements on a hollow cylinder in the von Karman Gas Dynamics Facility's 12-inch and 40-inch supersonic tunnels show that the highest transition Reynolds numbers were obtained in the 40-inch tunnel, although the variations with unit Reynolds number were the same at Mach numbers 3 to 5. The influence of nose bluntness in the 40-inch tunnel corresponds closely with the results obtained in the 12-inch tunnel.

Aeronautical Engineering

Aeronautical Engineering
Author:
Publisher:
Total Pages: 580
Release: 1971
Genre: Aeronautics
ISBN:

A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)

Handbook of Turbulence

Handbook of Turbulence
Author: Walter Frost
Publisher: Springer Science & Business Media
Total Pages: 511
Release: 2012-12-06
Genre: Technology & Engineering
ISBN: 1468423223

Turbulence takes place in practically all flow situations that occur naturally or in modern technological systems. Therefore, considerable effort is being expended in an attempt to understand this very complex physical phenome non and to develop both empirical and mathematical models for its description. Such numerical and analytical computational schemes would allow the reliable prediction and design of turbulent flow processes to be carried out. The purpose of this book is to bring together, in a usable form, some of the fundamental concepts of turbulence along with turbulence models and experimental techniques. It is hoped that these have "general applicability" in current engineering design. The phrase "general applicabil ity" is highlighted because the theory of turbulence is still so much in a formative stage that completely general analyses are not available now, nor will they be available in the immediate future. The concepts and models described herein represent the state-of-the art methods that are now being used to give answers to turbulent flow problems. As in all turbulent flow analysis, the methods are a blend of analytical and empirical input, and the reader should be cognizant of the simplification and restrictions imposed upon the methods when applyingthem to physical situations different from those for which they have been developed.

NASA Technical Paper

NASA Technical Paper
Author: United States. National Aeronautics and Space Administration
Publisher:
Total Pages: 44
Release: 1989
Genre: Aeronautics
ISBN: