- 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.
Search results
Showing 1 to 10 of 10 (0.088 seconds)Spelling suggestions: "subject:"supersonic wind tunnels"" "subject:"upersonic wind tunnels""
| 1 |
Initial Flow Calibration Results from the Florida Technological University four-inch supersonic wind tunnelBeck, James K. 01 January 1973 (has links) (PDF)
No description available.
|
| 2 |
Aspirating probes for measurement of mean concentration and fluctuating quantities in supersonic air/helium shear layer /Ninnemann, Todd A., January 1990 (has links)
Thesis (M.S.)--Virginia Polytechnic Institute and State University, 1990. / Vita. Abstract. Includes bibliographical references (leaves 61-62). Also available via the Internet.
|
| 3 |
The influences of artificially induced turbulence upon boundary-layer transition in supersonic flows /Olson, Lawrence Elroy January 1970 (has links)
No description available.
|
| 4 |
Investigation of an ion tracer technique for the measurement of supersonic air velocities.Schwartz, Hyman Harry. January 1971 (has links)
No description available.
|
| 5 |
Revitalization and initial testing of a blowdown supersonic wind tunnelRatliff, Card, January 2008 (has links)
Thesis (M.S.)--Mississippi State University. Department of Aerospace Engineering. / Title from title screen. Includes bibliographical references.
|
| 6 |
Investigation of an ion tracer technique for the measurement of supersonic air velocities.Schwartz, Hyman Harry. January 1971 (has links)
No description available.
|
| 7 |
Aspirating probes for measurement of mean concentration and fluctuating quantities in supersonic air/helium shear layerNinnemann, Todd A. 23 December 2009 (has links)
Two aspirating hot-film probes are developed to make measurements in supersonic air/helium shear layers. The first probe is designed to measure local mean gas composition and is referred to as the mean concentration probe. This probe consists of a constant temperature hot-film sensor operating in a channel with a choked exit. The flow over the hot-fifm is influenced only by total temperature, total pressure, and gas composition. The mean probe is easily calibrated and shows acceptable sensitivity to flow angularity. The second probe is based on an improved design of the mean concentration probe. In addition to measuring mean composition, this second probe also measures turbulence intensities of Reynolds number and thermal conductivity using a multiple overheat method. This probe is referred to as the turbulent probe. Both probes are used in the study of supersonic air/helium mixing layers in the VPI&SU 23 cmx23 cm Supersonic Wind Tunnel. Profiles of mean and turbulent quantities are presented. / Master of Science
|
| 8 |
Low-temperature supersonic flow control using repetitively pulsed MHD forceNishihara, Munetake, January 2006 (has links)
Thesis (Ph. D.)--Ohio State University, 2006. / Title from first page of PDF file. Includes bibliographical references (p. 114-120).
|
| 9 |
The design of a 3.4 by 3.4 inch supersonic wind tunnel capable of continuous operation in the range of Mach numbers between 1.50 and 3.59Anderson, Euell Clay January 1962 (has links)
Master of Science
|
| 10 |
Development of a supersonic wind tunnel rapid real-time data acquisition and control systemOkoro, Ndubuisi Emmanuel, January 2005 (has links)
Thesis (M.S.) -- Mississippi State University. Department of Aerospace Engineering. / Title from title screen. Includes bibliographical references.
|
Page generated in 0.0932 seconds