Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0, Jim A. Penland, James B. Hallissy, and James L. Dillon
Type
Label
Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0, Jim A. Penland, James B. Hallissy, and James L. Dillon
Language
eng
Bibliography note
Includes bibliographical references (pages 20-22)
resource.governmentPublication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary Form
non fiction
Main title
Aerodynamic characteristics of a hypersonic research airplane concept having a 70̊ swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0
Nature of contents
dictionariesbibliographytechnical reports
Responsibility statement
Jim A. Penland, James B. Hallissy, and James L. Dillon
Series statement
NASA technical paper, 1552
Contributor
Creator
Subject
Content
resource.issuingbody
Incoming Resources
- Has instance1
Outgoing Resources
- Contributor4
- Creator1
- Subject1
- Content1
- Author4
- resource.issuingbody1
- Other version1