contributor author | Stein Sture | |
contributor author | Nicholas C. Costes | |
contributor author | Susan N. Batiste | |
contributor author | Mark R. Lankton | |
contributor author | Khalid A. AlShibli | |
contributor author | Boris Jeremic | |
contributor author | Roy A. Swanson | |
contributor author | Melissa Frank | |
date accessioned | 2017-05-08T21:15:57Z | |
date available | 2017-05-08T21:15:57Z | |
date copyright | July 1998 | |
date issued | 1998 | |
identifier other | %28asce%290893-1321%281998%2911%3A3%2867%29.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/44875 | |
description abstract | Six displacement-controlled, conventional, drained axisymmetric triaxial experiments on cohesionless granular soil specimens were conducted at very low effective confining stresses in a SPACEHAB module on the Space Shuttle during the STS-79 and STS-89 missions. Three specimens were tested on each mission. The specimens measured 75 mm in diameter by 150 mm long. The average grain size of the subangular Ottawa quartz sand was 0.22 mm. The specimens' relative density for the STS-79 mission was 86.5% (±0.8%); for the STS-89 mission it was 65.0% (±1.0%). The confining stresses in the six experiments were 0.05, 0.52, and 1.30 kPa. Very high friction angles in the range of 47.6 to 70.0° were observed. The dilatancy angles were also unusually high, in the range of 30 to 31°. In spite of the very low effective stresses, high elastic moduli were observed. | |
publisher | American Society of Civil Engineers | |
title | Mechanics of Granular Materials at Low Effective Stresses | |
type | Journal Paper | |
journal volume | 11 | |
journal issue | 3 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)0893-1321(1998)11:3(67) | |
tree | Journal of Aerospace Engineering:;1998:;Volume ( 011 ):;issue: 003 | |
contenttype | Fulltext | |