Author: F. E. West
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32
Book Description
Force Test Results for Body-mounted Lateral Controls and Speed Brakes on a 45° Swept-wing Model at Mach Numbers from 0.80 to 0.98
Author: F. E. West
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 32
Book Description
Force Tests Results for Body-mounted Lateral Controls and Speed Brakes on a 45 Degree Swept-wing Model at Mach Numbers from 0.80 to 0.98
Author: F. E. West
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
An investigation has been made in the Langley 16-foot transonic tunnel to determine the aerodynamic characteristics of several body-mounted lateral-control and speed-brake configurations. The basic model had a 45 degree swept wing with an aspect ratio of 3. Six-component balance data were obtained at Mach numbers of 0.80, 0.94, and 0.98 for angles of attack that usually ranged from about zero to 21 degrees.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32
Book Description
An investigation has been made in the Langley 16-foot transonic tunnel to determine the aerodynamic characteristics of several body-mounted lateral-control and speed-brake configurations. The basic model had a 45 degree swept wing with an aspect ratio of 3. Six-component balance data were obtained at Mach numbers of 0.80, 0.94, and 0.98 for angles of attack that usually ranged from about zero to 21 degrees.
Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98
Author: F. E. West
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 76
Book Description
Effect of Body-Mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Deg Swept Wing at Mach Numbers from 0.80 to 0.98
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 80
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 80
Book Description
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1306
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1306
Book Description
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45 Degree Swept Wing at Mach Numbers from 0.80 to 0.98
Author: F. E. West
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
Effect of Body-mounted Lateral Controls and Speed Brakes on the Aerodynamic Load Distribution Over a 45° Swept Wing at Mach Numbers from 0.80 to 0.98
Author: F. E. West
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 72
Book Description
Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75°
Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38
Book Description
Introduction to Aircraft Flight Mechanics
Author: Thomas R. Yechout
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.