Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers / by Ivan E. Beckwith and James J. Gallagher.
Local heat transfer, equilibrium temperatures, and pressure have been measured on a circular cylinder for yaw angles from 0° to 60° and Reynolds numbers from 1X10⁶ to 4X10⁶. Increasing the yaw angle from 0° to 40° generally caused large increases in local heat-transfer coefficients followed by a dec...
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| Corporate Authors: | , |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration,
1961.
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| Series: | NASA technical report ;
R-104. |
| Subjects: |
MARC
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| 086 | 0 | |a NAS 1.12:104 | |
| 086 | 0 | |a NAS 1.12:104 | |
| 100 | 1 | |a Beckwith, Ivan E. |0 http://id.loc.gov/authorities/names/n82101336 |1 http://isni.org/isni/0000000023284158. | |
| 245 | 1 | 0 | |a Local heat transfer and recovery temperatures on a yawed cylinder at a mach number of 4.15 and high Reynolds numbers / |c by Ivan E. Beckwith and James J. Gallagher. |
| 260 | |a Washington, D.C. : |b National Aeronautics and Space Administration, |c 1961. | ||
| 300 | |a 25 pages : |b illustrations ; |c 26 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 NASA technical report ; |v R-104. | |
| 504 | |a Includes bibliographical references (page 25) | ||
| 520 | |a Local heat transfer, equilibrium temperatures, and pressure have been measured on a circular cylinder for yaw angles from 0° to 60° and Reynolds numbers from 1X10⁶ to 4X10⁶. Increasing the yaw angle from 0° to 40° generally caused large increases in local heat-transfer coefficients followed by a decrease as the yaw angle was increased to 60°. The level of heating rates and the type if chordwise distribution indicated that a flow mechanism different from the conventional transitional boundary layer may exist for the intermediate yaw angles. | ||
| 650 | 0 | |a Hypersonic planes. |0 http://id.loc.gov/authorities/subjects/sh85063718. | |
| 650 | 0 | |a Yawing (Aerodynamics) |0 http://id.loc.gov/authorities/subjects/sh85149046. | |
| 650 | 7 | |a Hypersonic planes. |2 fast |0 (OCoLC)fst00965814. | |
| 650 | 7 | |a Yawing (Aerodynamics) |2 fast |0 (OCoLC)fst01182552. | |
| 700 | 1 | |a Gallagher, James J. |0 http://id.loc.gov/authorities/names/n87903809. | |
| 710 | 2 | |a Langley Research Center. |0 http://id.loc.gov/authorities/names/n79134855 |1 http://isni.org/isni/0000000406376754. | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |0 http://id.loc.gov/authorities/names/n78087581 |1 http://isni.org/isni/0000000449071619. | |
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| 952 | f | f | |p Can circulate |a University of Colorado Boulder |b Boulder Campus |c Norlin |d Norlin Library - Government Information - US |e NAS 1.12:104 |h Superintendent of Documents classification |i document |m U183075212559 |n 1 |