Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing
Author: Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control
Author: Roger H. FournierPublisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 76
Book Description
An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.
Effect of Reynolds Number on the Low-speed Longitudinal Aerodynamic Characteristics of Two Variable-wing-sweep Airplane Configurations
Author: Aerodynamic Characteristics of Some Lifting Reentry Concepts Applicable to Transatmospheric Vehicle Design Studies
Author: NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2300
Book Description
NASA Technical Note
Author: A Selected Listing of NASA Scientific and Technical Reports for 1966
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2084
Book Description
Scientific and Technical Aerospace Reports
Author: Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1990
Book Description
Author: