|
|
|
|
| LEADER |
00000cam a2200000Ia 4500 |
| 001 |
b9005554 |
| 003 |
CoU |
| 008 |
101004e195207 ohua bt f000 0 eng d |
| 005 |
20231211212126.2 |
| 035 |
|
|
|a (OCoLC)ocn668082304
|
| 035 |
|
|
|a (OCoLC)668082304
|
| 040 |
|
|
|a LHL
|b eng
|c LHL
|d OCLCF
|d OCLCO
|d OCLCQ
|d COD
|
| 049 |
|
|
|a COD9
|
| 086 |
0 |
|
|a Y 3.N 21/5:6/2740
|
| 100 |
1 |
|
|a Maydew, R. C.
|q (Randall C.)
|0 http://id.loc.gov/authorities/names/n92025559
|1 http://isni.org/isni/0000000029782107.
|
| 245 |
1 |
0 |
|a Experimental investigation of the local and average skin friction in the laminar boundary layer on a flat plate at a Mach number of 2.4 /
|c Randall C. Maydew and Constantine C. Pappas.
|
| 260 |
|
|
|a Washington, D.C. :
|b National Advisory Committee for Aeronautics,
|c 1952.
|
| 300 |
|
|
|a 22 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. 2740.
|
| 500 |
|
|
|a "July 1952."
|
| 500 |
|
|
|a NACA TN Number 2740.
|
| 504 |
|
|
|a Includes bibliographical references.
|
| 520 |
3 |
|
|a Average and local skin-friction coefficients for laminar flow have been determined experimentally on a flat plate at a Mach number of 2.4 for a Reynolds number range of 720,000 to 2.800,000 and compared with a laminar-boundary-layer theory of Chapman and Rubesin. The average skin-friction data were considerably higher than values predicted by laminar-boundary-layer theory. Local skin-friction coefficients, evaluated by the two methods, agreed well with the theory when plotted against a momentum-thickness Reynolds.
|
| 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 Aerodynamics, Supersonic.
|0 http://id.loc.gov/authorities/subjects/sh85001297.
|
| 650 |
|
0 |
|a Laminar flow.
|0 http://id.loc.gov/authorities/subjects/sh85074205.
|
| 650 |
|
0 |
|a Laminar boundary layer.
|0 http://id.loc.gov/authorities/subjects/sh2003006140.
|
| 650 |
|
0 |
|a Skin friction (Aerodynamics)
|0 http://id.loc.gov/authorities/subjects/sh85123197.
|
| 650 |
|
0 |
|a Plates (Engineering)
|0 http://id.loc.gov/authorities/subjects/sh85103293.
|
| 650 |
|
7 |
|a Aerodynamics, Supersonic.
|2 fast
|0 (OCoLC)fst00798221.
|
| 650 |
|
7 |
|a Laminar boundary layer.
|2 fast
|0 (OCoLC)fst00991078.
|
| 650 |
|
7 |
|a Laminar flow.
|2 fast
|0 (OCoLC)fst00991079.
|
| 650 |
|
7 |
|a Plates (Engineering)
|2 fast
|0 (OCoLC)fst01066785.
|
| 650 |
|
7 |
|a Skin friction (Aerodynamics)
|2 fast
|0 (OCoLC)fst01120142.
|
| 700 |
1 |
|
|a Pappas, Constantine C.
|
| 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 2740.
|0 http://id.loc.gov/authorities/names/no2009017392.
|
| 907 |
|
|
|a .b90055548
|b 08-13-20
|c 01-27-17
|
| 998 |
|
|
|a pas
|b 01-27-17
|c r
|d m
|e -
|f eng
|g ohu
|h 0
|i 1
|
| 907 |
|
|
|a .b90055548
|b 10-25-19
|c 01-27-17
|
| 944 |
|
|
|a MARS - RDA ENRICHED
|
| 907 |
|
|
|a .b90055548
|b 02-01-17
|c 01-27-17
|
| 907 |
|
|
|a .b90055548
|b 01-27-17
|c 01-27-17
|
| 948 |
|
|
|a gro16/17:cjg
|
| 999 |
f |
f |
|i d12e2c14-871a-5c15-9d3f-d5b1ef37935c
|s 3c5a6a9f-00e8-5a39-a928-f1f41429970c
|
| 952 |
f |
f |
|p Can circulate
|a University of Colorado Boulder
|b Boulder Campus
|c Offsite
|d PASCAL Offsite
|e Y 3.N 21/5:6/2740
|h Superintendent of Documents classification
|i document
|m P204042108014
|n 1
|
