Two-dimensional approach to the maximum lift- to-drag ratio of a slender, flat-top, hypersonic wing

Two-dimensional approach to maximum lift-drag ratio of slender, flat-top, wing at hypersonic speeds

Document ID

19660010372

Acquisition Source

Legacy CDMS

Document Type

Contractor Report (CR)

Authors

Date Acquired

August 3, 2013

Publication Date

January 1, 1966

Subject Category

Report/Patent Number

Accession Number

66N19661

Funding Number(s)

Distribution Limits

Public

Work of the US Gov. Public Use Permitted.

Keywords

Name

Type

STI

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