Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /

Bibliographic Details

Main Authors:	Penland, Jim A. (Author), Hallissy, James B. (Author), Dillon, James L. (Author)
Corporate Author:	Langley Research Center (Author)
Format:	Government Document eBook
Language:	English
Published:	Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979.
Series:	NASA technical paper ; 1552.
Subjects:	Aerodynamics. Aerodynamic characteristics. Computational fluid dynamics. Delta wings. Hypersonic aircraft. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo52191