skip to content
INVISCID HYPERSONIC FLOW FOR POWER-LAW SHOCK WAVES. Preview this item
ClosePreview this item
Checking...

INVISCID HYPERSONIC FLOW FOR POWER-LAW SHOCK WAVES.

Author: Jr James T Lee; TRW SPACE TECHNOLOGY LABS REDONDO BEACH CA.
Publisher: Ft. Belvoir : Defense Technical Information Center, 16 APR 1963.
Edition/Format:   eBook : English
Database:WorldCat
Summary:
The blast wave solutions for the axisymmetric flow fields associated with a family of power law shocks, y sub s equals approximately x to the n power, were modified to properly account for the entropy layer near the surface of the body. The method of inner and outer expansions was used. It was shown that this method is of limited usefulness for n only slightly greater than 1/2 due to the slow convergence of the  Read more...
Rating:

(not yet rated) 0 with reviews - Be the first.

Subjects
More like this

 

Find a copy online

Links to this item

Find a copy in the library

&AllPage.SpinnerRetrieving; Finding libraries that hold this item...

Details

Material Type: Internet resource
Document Type: Internet Resource
All Authors / Contributors: Jr James T Lee; TRW SPACE TECHNOLOGY LABS REDONDO BEACH CA.
OCLC Number: 227312429
Description: 32 p. ; 23 x 29 cm.

Abstract:

The blast wave solutions for the axisymmetric flow fields associated with a family of power law shocks, y sub s equals approximately x to the n power, were modified to properly account for the entropy layer near the surface of the body. The method of inner and outer expansions was used. It was shown that this method is of limited usefulness for n only slightly greater than 1/2 due to the slow convergence of the inner expansions, but for (gamma 2)/(3 gamma 2) less than or equal to n <1 the expansions converge rapidly enough for the method to be useful. The case n 1/2 is singular and causes no difficulty. In the range (gamma 1) /(2 gamma 1) less than or equal to n<1 the body shape given by blast wave theory is correct, but the blast wave flow profiles must be modified near the body.

Reviews

User-contributed reviews
Retrieving GoodReads reviews...
Retrieving DOGObooks reviews...

Tags

Be the first.
Confirm this request

You may have already requested this item. Please select Ok if you would like to proceed with this request anyway.

Linked Data


<http://www.worldcat.org/oclc/227312429>
library:oclcnum"227312429"
library:placeOfPublication
library:placeOfPublication
owl:sameAs<info:oclcnum/227312429>
rdf:typeschema:Book
rdfs:seeAlso
schema:about
schema:about
schema:about
schema:about
schema:about
schema:about
schema:about
schema:about
schema:bookFormatschema:EBook
schema:contributor
schema:contributor
rdf:typeschema:Organization
schema:name"TRW SPACE TECHNOLOGY LABS REDONDO BEACH CA."
schema:datePublished"16 APR 1963"
schema:datePublished"1963"
schema:description"The blast wave solutions for the axisymmetric flow fields associated with a family of power law shocks, y sub s equals approximately x to the n power, were modified to properly account for the entropy layer near the surface of the body. The method of inner and outer expansions was used. It was shown that this method is of limited usefulness for n only slightly greater than 1/2 due to the slow convergence of the inner expansions, but for (gamma 2)/(3 gamma 2) less than or equal to n <1 the expansions converge rapidly enough for the method to be useful. The case n 1/2 is singular and causes no difficulty. In the range (gamma 1) /(2 gamma 1) less than or equal to n<1 the body shape given by blast wave theory is correct, but the blast wave flow profiles must be modified near the body."
schema:exampleOfWork<http://worldcat.org/entity/work/id/137053622>
schema:inLanguage"en"
schema:name"INVISCID HYPERSONIC FLOW FOR POWER-LAW SHOCK WAVES."
schema:numberOfPages"32"
schema:publisher
rdf:typeschema:Organization
schema:name"Defense Technical Information Center"
schema:url<http://handle.dtic.mil/100.2/AD406459>

Content-negotiable representations

Close Window

Please sign in to WorldCat 

Don't have an account? You can easily create a free account.