Mach number effects on turbine blade transition length prediction / R.J. Boyle and F.F. Simon.
Saved in:
| Online Access: |
Online Access Online Access |
|---|---|
| Main Authors: | , |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Cleveland, Ohio :
National Aeronautics and Space Administration, Lewis Research Center,
June 1998.
|
| Series: | NASA technical memorandum ;
208404. |
| Subjects: |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | b9249465 | ||
| 003 | CoU | ||
| 006 | m o d f | ||
| 007 | cr b|||||||||| | ||
| 008 | 170727e199806 ohua obt f000 0 eng c | ||
| 005 | 20230814214336.0 | ||
| 035 | |a (OCoLC)ocn995164631 | ||
| 040 | |a GPO |b eng |e rda |e pn |c GPO |d MvI | ||
| 042 | |a pcc | ||
| 049 | |a GDWR | ||
| 074 | |a 0830-D (online) | ||
| 086 | 0 | |a NAS 1.15:208404 | |
| 088 | |a 98-GT-367 | ||
| 100 | 1 | |a Boyle, Robert J., |e author. |0 http://id.loc.gov/authorities/names/n82229388 | |
| 245 | 1 | 0 | |a Mach number effects on turbine blade transition length prediction / |c R.J. Boyle and F.F. Simon. |
| 264 | 1 | |a Cleveland, Ohio : |b National Aeronautics and Space Administration, Lewis Research Center, |c June 1998. | |
| 300 | |a 1 online resource (12 pages) : |b illustrations. | ||
| 336 | |a text |b txt |2 rdacontent. | ||
| 337 | |a computer |b c |2 rdamedia. | ||
| 338 | |a online resource |b cr |2 rdacarrier. | ||
| 490 | 1 | |a NASA/TM ; |v 1998-208404 | |
| 500 | |a "June 1998." | ||
| 500 | |a "Prepared for the Turbo Expo '98 sponsored by the American Society of Mechanical Engineers, Stockholm, Sweden, June 2-5, 1998." | ||
| 500 | |a "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page. | ||
| 504 | |a Includes bibliographical references (pages 11-12) | ||
| 500 | |a "98-GT-367." | ||
| 513 | |a Technical memorandum. | ||
| 588 | |a Description based on online resource; title from PDF title page (NASA, viewed July 27, 2017) | ||
| 536 | |a Sponsored by the National Aeronautics and Space Administration |d WU-523-26-13-00 |d E-11237. | ||
| 650 | 7 | |a Mach number. |2 nasat | |
| 650 | 7 | |a Turbine blades. |2 nasat | |
| 650 | 7 | |a Mathematical models. |2 nasat | |
| 650 | 7 | |a Turbulence models. |2 nasat | |
| 650 | 7 | |a Navier-Stokes equation. |2 nasat | |
| 650 | 7 | |a Boundary layer transition. |2 nasat | |
| 700 | 1 | |a Simon, F. F. |q (Frederick F.), |e author. |0 http://id.loc.gov/authorities/names/no2011006750 | |
| 710 | 2 | |a Lewis Research Center, |e issuing body. |0 http://id.loc.gov/authorities/names/n80126316 |1 http://isni.org/isni/0000000406376607 | |
| 776 | 0 | 8 | |i Microfiche version: |a Boyle, Robert J. |t Mach number effects on turbine blade transition length prediction |w (OCoLC)41578841. |
| 830 | 0 | |a NASA technical memorandum ; |v 208404. |0 http://id.loc.gov/authorities/names/n83707893 | |
| 856 | 4 | 0 | |u https://purl.fdlp.gov/GPO/gpo83126 |z Online Access |
| 856 | 4 | 0 | |u http://purl.access.gpo.gov/GPO/gpo83126 |z Online Access |
| 907 | |a .b92494651 |b 06-12-23 |c 08-10-17 | ||
| 944 | |a MARS - RDA ENRICHED | ||
| 998 | |a web |b 08-10-17 |c - |d m |e - |f eng |g ohu |h 0 |i 2 | ||
| 948 | |a bslw22/23 : jun : ess (never sent) | ||
| 999 | f | f | |i 1bced165-e4e6-5e85-8eb6-020fbd1c057a |s f065b047-b284-5aea-8664-7feb075bd2b0 |
| 952 | f | f | |p Can circulate |a University of Colorado Boulder |b Online |c Online |d Online |e NAS 1.15:208404 |h Superintendent of Documents classification |i web |n 1 |