The effects of boundary-layer removal through throat slots on the internal performance of a side inlet at Mach numbers of 2.0 and 2.3

Wind tunnel study of boundary-layer-control throat bleed slot variations on internal performance of side inlet at Mach numbers 2.0 and 2.3

Document ID

19660010440

Acquisition Source

Legacy CDMS

Document Type

Technical Memorandum (TM)

Authors

Date Acquired

September 2, 2013

Publication Date

March 1, 1961

Subject Category

Report/Patent Number

Accession Number

66N19729

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

Name

Type

STI

No Preview Available

NTRS