USAAVLABS technical reports. 68-34. Study of high-Mach-number, high-temperature application of small, single-stage, axial-flow gas turbine [with bibliography]; by D. H. Cooke.
Publication Title:
Study of high-Mach-number, high-temperature application of small, single-stage, axial-flow gas turbine [with bibliography]; by D. H. Cooke.
Display Title:
USAAVLABS technical reports. 68-34. Study of high-Mach-number, high-temperature application of small, single-stage, axial-flow gas turbine [with bibliography]; by D. H. Cooke.
Series Title:
USAAVLABS technical reports.
Corporate Agency Authors:
Army Department and Defense Dept.
Sort Author:
Army Department
Authors:
Cooke, D. H.
Author place:
Washington, DC
Author zip:
20310
Date:
June 1968
Publish Date ISO Format:
1968-06-01T00:00:00Z
Publication Start:
19680601
Publication End:
19680630
Corporate/Agency Author:
Army Department
Publication month:
7
Publication year:
1968
SuDoc number:
D 117.8/2:(nos.)
Description:
[1]+ix+79+[2] p. il. 4°
Notes:
(Task 1M1259O1A01409. contract DAAJ02-67-C-0011; Rocketdyne technical report R-7261.) [Prepared by Rocketdyne, Division of North American Rockwell Corporation, Canoga Park, Calif.] and (Army Aviation Materiel Laboratories, Fort Eustis, Va.)
Notes:
(Army Aviation Materiel Laboratories, Fort Eustis, Va.) ‡ Official Use. Not Available.