The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 /
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| Author / Creator: | Burbank, Paige B., author. |
|---|---|
| Imprint: | Washington, [D.C.] : National Advisory Committee for Aeronautics, 1953. |
| Description: | 1 online resource (37 pages) : illustrations. |
| Language: | English |
| Series: | Technical notes / National Advisory Committee for Aeronautics ; No. 2921 Technical note (United States. National Advisory Committee for Aeronautics) ; 2921. |
| Subject: | |
| Format: | E-Resource U.S. Federal Government Document Book |
| URL for this record: | http://pi.lib.uchicago.edu/1001/cat/bib/12381211 |
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| 100 | 1 | |a Burbank, Paige B., |e author. | |
| 245 | 1 | 4 | |a The aerodynamic design and calibration of an asymmetric variable Mach number nozzle with a sliding block for the Mach number range 1.27 to 2.75 / |c by Paige B. Burbank and Robert W. Byrne. |
| 264 | 1 | |a Washington, [D.C.] : |b National Advisory Committee for Aeronautics, |c 1953. | |
| 300 | |a 1 online resource (37 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent |0 http://id.loc.gov/vocabulary/contentTypes/txt | ||
| 337 | |a computer |b c |2 rdamedia |0 http://id.loc.gov/vocabulary/mediaTypes/c | ||
| 338 | |a online resource |b cr |2 rdacarrier |0 http://id.loc.gov/vocabulary/carriers/cr | ||
| 490 | 1 | |a Technical notes / National Advisory Committee for Aeronautics ; |v No. 2921 | |
| 588 | |a Description based on online resource, PDF version; title from title page (TRAIL, viewed July 31, 2020). | ||
| 500 | |a "April 1953." | ||
| 500 | |a No Federal Depository Library Program (FDLP) item number. | ||
| 504 | |a Includes bibliographical references (page 11). | ||
| 650 | 0 | |a Nozzles |x Fluid dynamics. |0 http://id.loc.gov/authorities/subjects/sh85092917 | |
| 650 | 0 | |a Mach number. |0 http://id.loc.gov/authorities/subjects/sh85079305 | |
| 650 | 0 | |a Supersonic nozzles |x Design and construction. | |
| 650 | 7 | |a Mach number. |2 fast |0 (OCoLC)fst01004756 | |
| 650 | 7 | |a Nozzles |x Fluid dynamics. |2 fast |0 (OCoLC)fst01039829 | |
| 650 | 7 | |a Supersonic nozzles |x Design and construction. |2 fast |0 (OCoLC)fst01138998 | |
| 700 | 1 | |a Byrne, Robert W., |e author. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics, |e issuing body. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://viaf.org/viaf/136563305 | |
| 776 | 0 | 8 | |i Print version: |a Burbank, Paige B., |t Aerodynamic design and calibration of an asymmetric variable Mach number nozzle with sliding block for the Mach number range 1.27 to 2.75 |w (OCoLC)669625364 |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 2921. | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo142379 |y Government Publishing Office |
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| 929 | |a eresource | ||
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| 928 | |t Library of Congress classification |l Online |c UC-FullText |u https://purl.fdlp.gov/GPO/gpo142379 |z Government Publishing Office |g ebooks |i 11981322 | ||