Cover Image

Effect of forebody strakes on the aerodynamic characteristics in pitch and sideslip of a hypersonic airplane configuration at Mach numbers of 1.41, 2.01, and 6.86 /

Bibliographic Details
Main Author: Driver, Cornelius (Author)
Format: Government Document eBook
Language:English
Published: Washington : National Aeronautics and Space Administration, September 1959.
Series:NASA technical memorandum ; X-116.
Subjects:
Hypersonic aircraft.
Aerodynamic characteristics.
Aerodynamics.
Aerodynamic measurements.
Mach number.
Hypersonic planes.
Wind tunnel testing.
Shells (Engineering)
Noses (Aircraft)
Online Access:https://purl.fdlp.gov/GPO/gpo182854

Internet

https://purl.fdlp.gov/GPO/gpo182854