An Anomaly in the Resistivity-temperature Profile of Ultrapure Phenanthrene
Author: Paul A. Andrews
Publisher:
Published: 1965
Total Pages: 14
ISBN-13:
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Author: Paul A. Andrews
Publisher:
Published: 1965
Total Pages: 14
ISBN-13:
DOWNLOAD EBOOKAuthor: M. M. Borisenko
Publisher:
Published: 1968
Total Pages: 24
ISBN-13:
DOWNLOAD EBOOKThe paper considers profiles of wind velocities in the boundary layer computed from measurements of high towers in West Germany, England, Australia, the United States (Cedar Hill, Texas), Japan, and the USSR.
Author: United States. Department of the Treasury. Office of Procurement
Publisher:
Published: 1986
Total Pages: 78
ISBN-13:
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Publisher: IICA Biblioteca Venezuela
Published:
Total Pages: 32
ISBN-13:
DOWNLOAD EBOOKAuthor: United States. Office of Federal Contract Compliance Programs
Publisher:
Published: 1990
Total Pages: 1110
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DOWNLOAD EBOOKAuthor: Henry T. Wang
Publisher:
Published: 1971
Total Pages: 44
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DOWNLOAD EBOOKAuthor: Lawrence K. Waters
Publisher:
Published: 1967
Total Pages: 20
ISBN-13:
DOWNLOAD EBOOKSeven-week test-retest correlations were obtained for need scale scores and individual need profiles for a sample of pre-flight students. The coefficients for need scales were in the 50's and 60's (2 of 15 were below .50). Mean scores on 7 of the need scales changed significantly over the seven-week intertest interval. Of the 74 individual profile correlations, 64 were significant; the median value was .75. There was some evidence that low profile stability was related to a low consistency score on one or both administrations. The test-retest data were compared with other reliability studies of the Personal Preference Schedule. (Author).
Author: Roland E. Lee
Publisher:
Published: 1969
Total Pages: 114
ISBN-13:
DOWNLOAD EBOOKThe results of a detailed experimental investigation of a two- dimensional turbulent boundary layer at zero-pressure gradient are presented. The studies were made at the free-stream Mach number of 5, momentum-thickness Reynolds number from 4800 to 56,000 and wall-to-adiabatic-wall temperature ratios from 0.5 to 1.0. The data are in analytical terms of velocity profile, temperature profile, law-of-the-wall, velocity-defect law and incompressible form factor. Comparisons of local skin-friction coefficients obtained by four different experimental methods are shown. An empirical equation was derived from the shear-balance data to calculate the friction coefficient from known values of Mach number, heat transfer and Reynolds number.
Author: James F. Morrissey
Publisher:
Published: 1965
Total Pages: 20
ISBN-13:
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