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  • About
  • The Global ETD Search service is a free service for researchers to find electronic theses and dissertations. This service is provided by the Networked Digital Library of Theses and Dissertations.
    Our metadata is collected from universities around the world. If you manage a university/consortium/country archive and want to be added, details can be found on the NDLTD website.
11

An analysis of experiments on aerodynamic heating of high-velocity missiles in accelerated flight

Low, Ward Call January 1955 (has links)
Thesis (Ph.D.)--Boston University. / An analysis is given which treats experimental heat-transfer data obtained during flights of three V-2 rockets and two Aerobee rockets. This work was conducted largely at Boston University under Air Force Contracts W28-099-ac-395 and AF 33(615)-382. The instrumentation and rocket-flight phases extended from 1947 to 1952, while the analysis was carried out in the period from 1953 to 1955. A total of nine V-2 rockets were instrumented to some extent for the purposes of this experiment. The missiles for which data have been analyzed were chosen on the basis of best performance on the part of both instrumentation and rocket. Experimental equipment of special design was produced and installed by the Boston University group in the rockets which were launched in the White Sands area in New Mexico. Extensive field trips were required in this connection, both for the experiment on heat0transer and others in which the same group participated at the same time. The general program was one of research in physics of the upper atmosphere. Since the conclusion of the supporting contracts in October of 1954, additional consideration of the experimental results has continued on a private basis. The data obtained during the course of the present experiment were in the form of temperature variations as experienced by heat meters which were placed at selected locations over the body and fin of the rockets. The heat meters were small circular diaphragms of stainless steel which were placed flush with the rocket skin. Each diaphragm had on its central inner surface a pair of resistance thermometers made of nickel wire, with a diameter of 0.002". The thermometers were switched in sequence into a resistance bridge. One thermometer had always a higher resistance than the other, an arrangement which served two purposes. Firstly, the two values of voltage for a given temperature permited unambiguous determination of the direction in which the resistance bridge was unbalanced. Secondly, these two values of voltage were handled independently by our own instrumentation, and by the recording or telemetry devices. When two such different values of voltage were finally translated back into their equivalent temperatures, close agreement of the temperature values lent considerable support to their accuracy. When the two thermometers reported temperatures which were significantly different from each other, restraint was indicated in trusting their accuracy. Fortunately, close agreement of temperatures reported by the dual thermometers was the more usual experience. [TRUNCATED]
12

The interaction of sound with turbulent flow.

Succi, George P January 1977 (has links)
Thesis. 1977. Ph.D. cn--Massachusetts Institute of Technology. Dept. of Physics / Vita. / Includes bibliographical references. / Ph.D.cn
13

Validation of software for the calculation of aerodynamic coefficients : with a focus on the software package Tornado

López Pereira, Ramón January 2010 (has links)
No description available.
14

Studies in aeroacoustics of coaxial vortex rings

梁志堅, Leung, Chi-kin, Randolph. January 1997 (has links)
published_or_final_version / abstract / toc / Mechanical Engineering / Doctoral / Doctor of Philosophy
15

A method of determining the cowl drag of an isolated ducted fan in an incompressible flow

Drummond, James E. January 1962 (has links)
No description available.
16

A method to separate wind-tunnel background noise and wind noise from interior measurements

Stoker, Robert W. 05 1900 (has links)
No description available.
17

The analysis of wing loads in roller coaster maneuvers

Rees, Pembroke Graves 08 1900 (has links)
No description available.
18

A study of heat release rate distribution in open premixed turbulent flames by acoustic measurements

Ramachandra, Manjanatha Kumar 08 1900 (has links)
No description available.
19

A methodology for robust structural design with application to active aeroelastic wings

Zink, Paul Scott 08 1900 (has links)
No description available.
20

Development of an efficient and versatile panel method for aerodynamic problems

Petrie, J. A. H. January 1979 (has links)
No description available.

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