Welcome to the Kids' Library!
Search for books, movies, music, magazines, and more.
Your session will expire automatically in
0
seconds.
Continue session
End session now
Back to Search Results
SearchType
Keyword
Author
Title
Subject
Call Number
Alternate Subject
Search
Search Scope
PSU Library Consortium
Pittsburg State University
Academic Libraries
Public Libraries
Pittsburg Area
Unified School District
Leonard H. Axe Library
Career Resource Center Library
Eureka Public Library
Fort Scott Community College Library
George Nettels Elementary School Library
Kansas Technology Center Library
Lakeside Elementary School Library
Meadowlark Elementary School Library
Parsons Public Library
Pittsburg Community Middle School Library
Pittsburg High School Library
Pittsburg Public Library
Sedan Public Library
Westside Elementary School Library
Childrens Collection
Available items only
Record 13 of 14
Previous Record
Next Record
Author
Ashby, George C., author.
Title
A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 / George C. Ashby, Jr.
Publication Info.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980.
Connect to
Connect to https://ntrs.nasa.gov/citations/19810005404
Copies
Location
Call No.
OPAC Message
Status
Axe Federal Documents Online
NAS 1.60:1787
---
Available
Description
1 online resource (31 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series
NASA technical paper ; 1787
NASA technical paper ; 1787.
Note
Title from title screen (viewed on Aug. 23, 2016).
"December 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography
Includes bibliographical references (page 9).
Type Of Report
Technical paper.
Funding
National Aeronautics and Space Administration 506-51-13-02 L-14017
Subject
Sonic boom.
Aerodynamics, Supersonic.
Aerodynamics, Supersonic. (OCoLC)fst00798221
Sonic boom. (OCoLC)fst01126586
Blunt bodies.
Far fields.
Finite Difference Theory.
Sonic booms.
Static pressure.
Genre/Form
Online resources.
Electronic books.
Electronic government information.
Added Author
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other Form:
Print version: Ashby, George C. Study of the sonic-boom characteristics of a blunt body at a Mach number of 6 (OCoLC)7499601
Gpo Item No.
0830-H-15 (online)
Sudoc No.
NAS 1.60:1787
Available items only
