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Engineering considerations on the transversal contour of a lifting body.

Authors :
Huang, H.-Y
Miele, A
Publication Year :
1967
Publisher :
United States: NASA Center for Aerospace Information (CASI), 1967.

Abstract

Lift drag ratios attainable by slender bodies at hypersonic speeds assuming modified Newtonian pressure distribution and surface constant friction coefficient

Subjects

Subjects :
Aircraft

Details

Language :
English
Database :
NASA Technical Reports
Notes :
NGR-44-006-063
Publication Type :
Report
Accession number :
edsnas.19680041379
Document Type :
Report

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