Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing PDF full book. Access full book title Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing by . Download full books in PDF and EPUB format.

Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing

Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54

Get Book Here

Book Description

Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing

Effects of Reynolds Number at Low Subsonic Speeds on Aerodynamic Characteristics of a Reentry Body with a Variable Sweep Wing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54

Get Book Here

Book Description

Effect of Reynolds Number on the Low-speed Longitudinal Aerodynamic Characteristics of Two Variable-wing-sweep Airplane Configurations

Effect of Reynolds Number on the Low-speed Longitudinal Aerodynamic Characteristics of Two Variable-wing-sweep Airplane Configurations PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

Get Book Here

Book Description

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

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 PDF Author: Roger H. Fournier
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 76

Get Book Here

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.

Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds

Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds PDF Author: William P. Henderson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60

Get Book Here

Book Description

Aerodynamic Characteristics of Some Lifting Reentry Concepts Applicable to Transatmospheric Vehicle Design Studies

Aerodynamic Characteristics of Some Lifting Reentry Concepts Applicable to Transatmospheric Vehicle Design Studies PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

Get Book Here

Book Description

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 836

Get Book Here

Book Description

Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds

Effects of Sweep Angle on the Boundary-layer Stability Characteristics of an Untapered Wing at Low Speeds PDF Author: Frederick W. Boltz
Publisher:
ISBN:
Category :
Languages : en
Pages : 84

Get Book Here

Book Description

Low-speed, Full-scale Reynolds Number Investigation of the Effects of Wing Leading-edge Radius, Elevons, Landing Gear, and a Body Flap on the Static Longitudinal Aerodynamic Characteristics of a Winged Reentry Configuration

Low-speed, Full-scale Reynolds Number Investigation of the Effects of Wing Leading-edge Radius, Elevons, Landing Gear, and a Body Flap on the Static Longitudinal Aerodynamic Characteristics of a Winged Reentry Configuration PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

Get Book Here

Book Description

Hypersonic Aerodynamic Characteristics of a Lifting Reentry Vehicle Model with Four Types of Longitudinal Control Surfaces

Hypersonic Aerodynamic Characteristics of a Lifting Reentry Vehicle Model with Four Types of Longitudinal Control Surfaces PDF Author: Charles Trescot (D. Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 52

Get Book Here

Book Description

Effects of Wing Leading-edge Radius and Reynold Number on Longitudinal Aerodynamic Characteristics of Highly Swept Wing-body Configurations at Subsonic Speeds

Effects of Wing Leading-edge Radius and Reynold Number on Longitudinal Aerodynamic Characteristics of Highly Swept Wing-body Configurations at Subsonic Speeds PDF Author: William P. Henderson
Publisher:
ISBN:
Category :
Languages : en
Pages : 53

Get Book Here

Book Description