CaltechAUTHORS
  A Caltech Library Service

Transient rocket-engine gas flow in soil

Ko, H.-Y. and Scott, R. F. (1968) Transient rocket-engine gas flow in soil. AIAA Journal, 6 (2). pp. 258-264. ISSN 0001-1452. https://resolver.caltech.edu/CaltechAUTHORS:20151208-153233282

[img] PDF - Published Version
See Usage Policy.

2MB

Use this Persistent URL to link to this item: https://resolver.caltech.edu/CaltechAUTHORS:20151208-153233282

Abstract

As a result of an examination of the behavior of soils subjected to rocket and jet exhaust gases. it was concluded that the gas pressure in the pores of the soil played an important part in the process of soil removal which occurred. Consequently, a numerical study of axially symmetric isothermal nonlinear gas flow ill a porous medium was undertaken. The paper presents the results and interpretations of the calculations for the particular boundary pressure conditions developed by a Surveyor spacecraft vernier engine mounted 12 in, above a granular material.


Item Type:Article
Related URLs:
URLURL TypeDescription
http://dx.doi.org/10.2514/3.4487DOIArticle
http://arc.aiaa.org/doi/abs/10.2514/3.4487PublisherArticle
Additional Information:© 1968 AIAA. Received February 20, 1967; revision received July 2 , 1967. The analytical work described in this paper was supported under California Institute of Technology, Jet Propulsion Laboratory, Engineering Contract 69811.
Funders:
Funding AgencyGrant Number
Caltech/JPL69811
Issue or Number:2
Record Number:CaltechAUTHORS:20151208-153233282
Persistent URL:https://resolver.caltech.edu/CaltechAUTHORS:20151208-153233282
Official Citation: H.-Y. KO and R. F. SCOTT. "Transient rocket-engine gas flow in soil." AIAA Journal, Vol. 6, No. 2 (1968), pp. 258-264. doi: 10.2514/3.4487
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:62723
Collection:CaltechAUTHORS
Deposited By: Ruth Sustaita
Deposited On:09 Dec 2015 00:05
Last Modified:03 Oct 2019 09:21

Repository Staff Only: item control page