Relative performance comparison between baseline labyrinth and dual-brush compressor discharge seals in a T-700 engine test
By: Robert C. Hendricks ... [et al.].
Contributors: Hendricks, Robert C.; United States. National Aeronautics and Space Administration.; U.S. Army Research Laboratory.
Series: NASA technical memorandum -- 106360.; Army Research Laboratory memorandum report -- ARL-MR-232.
Publisher: National Aeronautics and Space Administration; U.S. Army Research Laboratory; National Technical Information Service, distributor
Published: 1995
Place of publication: [Washington, D.C.]; [Adelphi, Md.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Air flow.; Brush seals.; Compressors.; Engine tests.; Labyrinth seals.; Secondary flow.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 1 microfiche.