Cover Image

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
Description
Item Description:Title from title screen (viewed Sept. 22, 2014).
"December 1979."
"Performing organization, NASA Langley Research Center"--Technical report documentation page.
Physical Description:1 online resource (144 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 20-22).