Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions / L.W. Florschuetz, D.E. Metzger, and C.R. Truman.
Correlations for heat transfer coefficients for jets of circular offices and impinging on a surface parallel to the jet orifice plate are presented. The air, following impingement, is constrained to exit in a single direction along the channel formed by the jet orifice plate and the heat transfer (i...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. : [Springfield, Va.] :
National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service],
1981.
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| Series: | NASA contractor report ;
NASA CR-3373. |
| Subjects: |
MARC
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| 100 | 1 | |a Florschuetz, L. W. |0 http://id.loc.gov/authorities/names/n81041553. | |
| 245 | 1 | 0 | |a Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions / |c L.W. Florschuetz, D.E. Metzger, and C.R. Truman. |
| 260 | |a Washington, D.C. : |b National Aeronautics and Space Administration, Scientific and Technical Information Branch ; |a [Springfield, Va.] : |b [For sale by the National Technical Information Service], |c 1981. | ||
| 300 | |a vi, 54 pages : |b illustrations ; |c 27 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 contractor report ; |v 3373. | |
| 500 | |a Jan. 1981. | ||
| 504 | |a Includes bibliographical references (pages 53-54) | ||
| 500 | |a "Prepared for Lewis Research Center under Grant NSG-3075." | ||
| 500 | |a "Arizona State University, Tempe." | ||
| 520 | |a Correlations for heat transfer coefficients for jets of circular offices and impinging on a surface parallel to the jet orifice plate are presented. The air, following impingement, is constrained to exit in a single direction along the channel formed by the jet orifice plate and the heat transfer (impingement) surface. The downstream jets are subjected to a crossflow originating from the upstream jets. Impingement surface heat transfer coefficients resolved to one streamwise jet orifice spacing, averaged across the channel span, are correlated with the associated individual spanwise orifice row jet and crossflow velocities, and with the geometric parameters. (NTRL site) | ||
| 650 | 0 | |a Heat |x Transmission. |0 http://id.loc.gov/authorities/subjects/sh85059767. | |
| 650 | 0 | |a Aerofoils. |0 http://id.loc.gov/authorities/subjects/sh85001301. | |
| 650 | 0 | |a Aircraft gas-turbines. |0 http://id.loc.gov/authorities/subjects/sh85002744. | |
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| 700 | 1 | |a Metzger, Darryl E., |d 1937- |0 http://id.loc.gov/authorities/names/n83145329 |1 http://isni.org/isni/0000000081675915. | |
| 700 | 1 | |a Truman, C. R. |0 http://id.loc.gov/authorities/names/n81041561 |1 http://isni.org/isni/0000000023580483. | |
| 710 | 1 | |a United States. |b National Aeronautics and Space Administration. |b Scientific and Technical Information Branch. |0 http://id.loc.gov/authorities/names/n78091122. | |
| 710 | 2 | |a Lewis Research Center. |0 http://id.loc.gov/authorities/names/n80126316 |1 http://isni.org/isni/0000000406376607. | |
| 710 | 2 | |a Arizona State University. |0 http://id.loc.gov/authorities/names/n79034872 |1 http://isni.org/isni/0000000121512636. | |
| 776 | 0 | 8 | |i Online version: |a Florschuetz, L.W. |t Jet array impingement with crossflow - correlation of streamwise resolved flow and heat transfer distributions |w (OCoLC)761334290. |
| 830 | 0 | |a NASA contractor report ; |v NASA CR-3373. |0 http://id.loc.gov/authorities/names/n83825229. | |
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