Report of NRL Progress
Author : Naval Research Laboratory (U.S.)
Publisher :
Page : 168 pages
File Size : 12,92 MB
Release :
Category : Naval research
ISBN :
Author : Naval Research Laboratory (U.S.)
Publisher :
Page : 168 pages
File Size : 12,92 MB
Release :
Category : Naval research
ISBN :
Author : United States. Naval Research Laboratory, Washington
Publisher :
Page : 560 pages
File Size : 33,36 MB
Release : 1973
Category : Naval research
ISBN :
Author : Norman Chigier
Publisher : CRC Press
Page : 551 pages
File Size : 35,69 MB
Release : 2024-11-01
Category : Technology & Engineering
ISBN : 1040292305
The book begins with an introduction to the general problems of making measurements in high temperature and a presentation of chemically reacting flow systems. It describes each instrument with the various diagnostic techniques and discusses measurements that have been made in furnaces, flames, and rocket engines. The detailed measurement techniques described in this book cover a wide spectrum of applications in combustion systems, including gas turbine, rocket measurement techniques that were developed in laboratories. Information obtained on detailed temperature, velocity, particle size, and gas concentration distribution is leading to improve understanding of the chemical combustion process and to design imporvements in combustors.
Author :
Publisher :
Page : 80 pages
File Size : 31,45 MB
Release : 1976
Category : Aerodynamics
ISBN :
Author :
Publisher :
Page : 296 pages
File Size : 28,35 MB
Release : 1991
Category : Aeronautics
ISBN :
Author : Murray Tobak
Publisher :
Page : 76 pages
File Size : 13,35 MB
Release : 1976
Category : Nonlinear functional analysis
ISBN :
The theory of functionals is used to reformulate the notions of aerodynamic indicial functions and superposition. Integral forms for the aerodynamic response to arbitrary motions are derived that are free of dependence on a linearity assumption. Simplifications of the integral forms lead to practicable nonlinear generalizations of the linear superposition and the stability derivative formulations. Applied to arbitrary nonplanar motions, the generalization yields a form for the aerodynamic response that can be compounded of the contributions from a limited number of well-defined characteristic motions, in principle reproducible in the wind tunnel. Further generalizations that would enable the consideration of random fluctuations and multivalued aerodynamic responses are indicated.
Author : International Council of the Aeronautical Sciences. Congress
Publisher :
Page : 900 pages
File Size : 42,64 MB
Release : 1980
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 742 pages
File Size : 46,63 MB
Release : 1984
Category : Engineering
ISBN :
Author : Benjamin Chu
Publisher : Elsevier
Page : 333 pages
File Size : 46,5 MB
Release : 1974-01-01
Category : Science
ISBN : 032316255X
Laser Light Scattering
Author : R. L. P. Voisinet
Publisher :
Page : 88 pages
File Size : 10,89 MB
Release : 1974
Category : Fluid mechanics
ISBN :
The predominant probes used for measuring total temperature in a compressible boundary-layer flow are described. The results of a direct comparison between two of these probes, the conical equilibrium temperature probe (Danberg probe) and the combined temperature-pressure probe of the DFVLR-AVA, are presented. The comparison was made by testing the probes simultaneously in the nozzle-wall turbulent boundary-layer flow of the NOL Boundary Layer Channel at zero and moderate heat-transfer conditions...