Ribbon and gliding type parachutes evaluated in the 7 by 10 foot transonic wind tunnel [electronic resource]

Saved in:
Bibliographic Details
Online Access: Online Access
Corporate Author: Sandia National Laboratories (Researcher)
Format: Government Document Electronic eBook
Language:English
Published: Albuquerque, N.M. : Oak Ridge, Tenn. : Sandia National Laboratories. ; distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy, 1975.
Subjects:

MARC

LEADER 00000nam a22000003u 4500
001 b7223557
003 CoU
005 20120313000000.0
006 m d f
007 cr |||||||||||
008 120401e19750901nmu ot f0|||||eng|d
035 |a (TOE)ost7296181 
035 |a (TOE)7296181 
040 |a TOE  |c TOE 
049 |a GDWR 
072 7 |a 42  |2 edbsc 
086 0 |a E 1.99:sand-75-7072 
086 0 |a E 1.99:sand-75-7072 
088 |a sand-75-7072 
245 0 0 |a Ribbon and gliding type parachutes evaluated in the 7 by 10 foot transonic wind tunnel  |h [electronic resource] 
260 |a Albuquerque, N.M. :  |b Sandia National Laboratories. ;  |a Oak Ridge, Tenn. :  |b distributed by the Office of Scientific and Technical Information, U.S. Dept. of Energy,  |c 1975. 
336 |a text  |b txt  |2 rdacontent. 
337 |a computer  |b c  |2 rdamedia. 
338 |a online resource  |b cr  |2 rdacarrier. 
500 |a Published through the Information Bridge: DOE Scientific and Technical Information. 
500 |a 09/01/1975. 
500 |a "sand-75-7072" 
500 |a Ottensoser, J. 
500 |a Naval Ship Research and Development Center, Bethesda, Md. (USA). Aviation and Surface Effects Dept. 
520 3 |a An experiment has been conducted in the NSRDC 7- x 10-foot transonic tunnel for the Sandia Corporation to evaluate various parachute parameters. The experiment consisted of three main parts: the first phase evaluated the disreefing characteristics of the various parachutes as well as the drag forces before, during, and after disreefing; the second phase measured the pressure distribution around the chute as well as the drag forces; and the final phase evaluated the disreefing and drag characteristics of gliding type parachutes. The free stream dynamic pressure varied from 65 to 500 psf. 12 figures, 1 table. (auth) 
536 |b AT(29-1)-789. 
650 7 |a Testing.  |2 local. 
650 7 |a Parachutes.  |2 local. 
650 7 |a Functional Models.  |2 local. 
650 7 |a Fluid Flow.  |2 local. 
650 7 |a Tunnels.  |2 local. 
650 7 |a Transonic Flow.  |2 local. 
650 7 |a Wind Tunnels.  |2 local. 
650 7 |a Engineering.  |2 edbsc. 
710 2 |a Sandia National Laboratories.  |4 res. 
710 1 |a United States.  |b Department of Energy.  |b Office of Scientific and Technical Information.  |4 dst. 
856 4 0 |u http://www.osti.gov/servlets/purl/7296181/  |z Online Access 
907 |a .b72235573  |b 03-07-23  |c 11-08-12 
998 |a web  |b 11-08-12  |c f  |d m   |e p  |f eng  |g nmu  |h 0  |i 1 
956 |a Information bridge 
999 f f |i ef3878b8-16ea-5ae5-8ba8-30b6a981974a  |s 79ae54a3-2332-515b-903c-08cc4788b76c 
952 f f |p Can circulate  |a University of Colorado Boulder  |b Online  |c Online  |d Online  |e E 1.99:sand-75-7072  |h Superintendent of Documents classification  |i web  |n 1