WIND-TUNNEL INVESTIGATION OF THE STATIC STABILITY OF A 1 56-SCALE MODEL OF THE X-1E AIRPLANE AT MACH NUMBERS OF 2.37, 2.98, AND 4.01

Wind tunnel tests of static stability of model x-1e aircraft at mach 2 to 4

Document ID

19630003098

Acquisition Source

Legacy CDMS

Document Type

Technical Memorandum (TM)

Authors

Date Acquired

September 2, 2013

Publication Date

August 1, 1959

Subject Category

Report/Patent Number

Accession Number

63N12974

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

Name

Type

STI

No Preview Available

NTRS