Heat transfer to bodies in a high-speed rarefied-gas stream / Jackson R. Stalder, Glen Goodwin, and Marcus O. Creager.
The equilibrium temperature and heat-transfer coefficients for transverse cylinders in a high-speed stream of rarefied gase were measured over a range of Knudsen numbers for 0.025 to 11.8 for Mach numbers from 2.0 to 3.3. Fully developed free-molecule flow was found to first occur at Knudsen numbres...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | , |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1951.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2438. |
| Subjects: |
MARC
| LEADER | 00000cam a2200000Ia 4500 | ||
|---|---|---|---|
| 001 | b8961718 | ||
| 003 | CoU | ||
| 008 | 100922e195108 ohua bt f000 0 eng d | ||
| 005 | 20231211212844.1 | ||
| 035 | |a (OCoLC)ocn664828846 | ||
| 035 | |a (OCoLC)664828846 | ||
| 040 | |a LHL |b eng |c LHL |d OCLCO |d OCLCQ |d COD | ||
| 049 | |a COD9 | ||
| 086 | 0 | |a Y 3.N 21/5:6/2438 | |
| 100 | 1 | |a Stalder, Jackson R. | |
| 245 | 1 | 0 | |a Heat transfer to bodies in a high-speed rarefied-gas stream / |c Jackson R. Stalder, Glen Goodwin, and Marcus O. Creager. |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1951. | ||
| 300 | |a 25 pages : |b illustrations ; |c 28 cm. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a unmediated |b n |2 rdamedia. | ||
| 338 | |a volume |b nc |2 rdacarrier. | ||
| 490 | 1 | |a National Advisory Committee for Aeronautics. Technical Note ; |v no. 2438. | |
| 500 | |a "August 1951." | ||
| 500 | |a NACA TN Number 2438. | ||
| 504 | |a Includes bibliographical references. | ||
| 520 | 3 | |a The equilibrium temperature and heat-transfer coefficients for transverse cylinders in a high-speed stream of rarefied gase were measured over a range of Knudsen numbers for 0.025 to 11.8 for Mach numbers from 2.0 to 3.3. Fully developed free-molecule flow was found to first occur at Knudsen numbres from approximately 2.0. The Nusselt number was found to be a function of the Reynolds number only, and the temperature-recovery factor to depend primarily on the Knudsen number. | |
| 583 | 1 | |a committed to retain |c 20230101 |d 20480101 |5 CoU |f Alliance Shared Trust |u https://www.coalliance.org/shared-print-archiving-policies. | |
| 650 | 0 | |a Gas flow. |0 http://id.loc.gov/authorities/subjects/sh85053300. | |
| 650 | 0 | |a Temperature. |0 http://id.loc.gov/authorities/subjects/sh85133712. | |
| 650 | 0 | |a Heat |x Transmission. |0 http://id.loc.gov/authorities/subjects/sh85059767. | |
| 650 | 0 | |a Rarefied gas dynamics |x Measurements. | |
| 700 | 1 | |a Goodwin, Glen. |0 http://id.loc.gov/authorities/names/n85823728. | |
| 700 | 1 | |a Creager, Marcus O. | |
| 710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://isni.org/isni/0000000106642010. | |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 2438. |0 http://id.loc.gov/authorities/names/no2009017392. | |
| 907 | |a .b89617186 |b 08-13-20 |c 01-06-17 | ||
| 998 | |a pas |b 01-06-17 |c r |d m |e - |f eng |g ohu |h 0 |i 1 | ||
| 907 | |a .b89617186 |b 10-11-17 |c 01-06-17 | ||
| 944 | |a MARS - RDA ENRICHED | ||
| 907 | |a .b89617186 |b 01-13-17 |c 01-06-17 | ||
| 948 | |a gro16/17:cjg | ||
| 999 | f | f | |i 2c457ba5-dc9c-5335-97a6-df88ccf81004 |s 6490ead8-9389-5edb-86a0-60d9a057d545 |
| 952 | f | f | |p Can circulate |a University of Colorado Boulder |b Boulder Campus |c Offsite |d PASCAL Offsite |e Y 3.N 21/5:6/2438 |h Superintendent of Documents classification |i document |m P106231605016 |n 1 |