Flow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96

by Robert L. Weirich and Walter A. Vahl

Resource Type:: E-Book
Publication:: Washington, D.C. : National Aeronautics and Space Administration, October 1968
Related Series:: NASA technical note; D-4809

No items found. Please contact the Willis Library Service Desk for assistance

Author/Creator:: Weirich, Robert L. , author
Contributors:: Vahl, Walter A. , author
United States National Aeronautics and Space Administration , issuing body, http://id.loc.gov/vocabulary/relators/isb
Languages:: English
Language Notes:: Item content: English
Main Work:: Flow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96 [by Weirich, R.L.]
Other Related Resources:: Print version: Flow-field properties near an arrow-wing [by Weirich, R.L.] (OCLC Number 52342299)
Related Series:: NASA technical note; D-4809
Subjects:: Supersonic wind tunnels — Testing
Supersonic planes — Design and construction
Supersonic planes — Testing
Supersonic wind tunnels
Supersonic planes
Testing
General Notes:: "October 1968."
Includes bibliographical references (page 12).
Description based on online resource, PDF version; title from title page (NASA, viewed on Nov. 13, 2020).
Physical Description:: 1 online resource (135 pages) : illustrations.
Digital Characteristics:: text file
Call Numbers:: NAS 1.14:D-4809
SuDocs Numbers:: NAS 1.14:D-4809
Other Standard Numbers:: Government Printing Office Item Number: 0830-H-13 (online)
OCLC Numbers:: 761487580