Performance of two 10-lb/sec centrifugal compressors with different blade and shroud thicknesses operating over a range of Reynolds numbers [microform] / Gary J. Skoch and Royce D. Moore.
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Other title: | Performance of two ten-lb/sec centrifugal compressors with different blade and shroud thicknesses operating over a range of Reynolds numbers. |
Format: | Government Document Microfilm Book |
Language: | English |
Published: |
[Washington, DC] : Cleveland, Ohio : [Springfield, Va.] :
National Aeronautics and Space Administration ; U.S. Army Aviation R&T Activity ; [For sale by the National Technical Information Service],
[1987]
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Series: | NASA technical memorandum ;
100115. AVSCOM technical report ; 87-C-21. |
Subjects: |
MARC
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245 | 1 | 0 | |a Performance of two 10-lb/sec centrifugal compressors with different blade and shroud thicknesses operating over a range of Reynolds numbers |h [microform] / |c Gary J. Skoch and Royce D. Moore. |
260 | |a [Washington, DC] : |b National Aeronautics and Space Administration ; |a Cleveland, Ohio : |b U.S. Army Aviation R&T Activity ; |a [Springfield, Va.] : |b [For sale by the National Technical Information Service], |c [1987] | ||
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490 | 1 | |a NASA technical memorandum ; |v 100115. | |
490 | 1 | |a AVSCOM technical report ; |v 87-C-21. | |
500 | |a Distributed to depository libraries in microfiche. | ||
533 | |a Microfiche. |b [Washington, D.C.? : |c National Aeronautics and Space Administration], |d 1987. |e 1 microfiche. | ||
650 | 0 | |a Compressors. |0 http://id.loc.gov/authorities/subjects/sh85029444. | |
650 | 0 | |a Turbomachines. |0 http://id.loc.gov/authorities/subjects/sh85138741. | |
700 | 1 | |a Moore, Royce D. |0 http://id.loc.gov/authorities/names/n81086703. | |
710 | 1 | |a United States. |b Army Aviation Research and Technology Activity. |0 http://id.loc.gov/authorities/names/no90015738. | |
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. | |
740 | 0 | |a Performance of two ten-lb/sec centrifugal compressors with different blade and shroud thicknesses operating over a range of Reynolds numbers. | |
830 | 0 | |a NASA technical memorandum ; |v 100115. |0 http://id.loc.gov/authorities/names/n83707893. | |
830 | 0 | |a AVSCOM technical report ; |v 87-C-21. |0 http://id.loc.gov/authorities/names/n86719948. | |
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