Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Transonic Aerodynamic Characteristics at a Wing Sweep of 104 Deg of a Variable-sweep Airplane Configuration with an Over and Under Engine Installation
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Transonic Aerodynamic Characteristics at a Wing Sweep of 104 of a Variable Sweep Airplane Configuration with an Over and Under Engine Installation
Author: Robert J. Ward
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location
Author: Ralph P. Bielat
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 84
Book Description
Transonic Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having a 12-percent-thick Wing and an Inboard Pivot Location
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 44
Book Description
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746
Book Description
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1746
Book Description
The Transonic Aerodynamic Characteristics of Two Variable-sweep Airplane Configurations Capable of Low-level Supersonic Attack
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 54
Book Description
Transonic Investigation of Aerodynamic Characteristics of a Swept-wing Fighter-airplane Model with Leading-edge Droop in Combination with Outboard Chord-extensions and Notches
Author: Charles F. Whitcomb
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 34
Book Description
An investigation of the effects of several wing leading-edge modifications on the aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model has been conducted in the Langley 16-foot transonic tunnel at low and high lifting conditions at Mach numbers from 0.85 to 1.03. The investigation included the determination of the effect on longitudinal stability and performance characteristics of wing leading-edge and chord-extension droops of 6 and 20 degrees, chord-extension overhangs of 0.075c and 0.15c (where c is the wing chord), leading-edge notches cut out at the inboard end of the 0.075c chord-extension to depths of 0.075c and 0.125c, and indentation of the model fuselage to conform partially to the supersonic area rule for a Mach number of 1.20. Lift, drag, and pitching-moment data were obtained for configurations with the tail on and off. Comparisons of data obtained from the present model with data from a configuration with leading-edge slats are included.
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 34
Book Description
An investigation of the effects of several wing leading-edge modifications on the aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model has been conducted in the Langley 16-foot transonic tunnel at low and high lifting conditions at Mach numbers from 0.85 to 1.03. The investigation included the determination of the effect on longitudinal stability and performance characteristics of wing leading-edge and chord-extension droops of 6 and 20 degrees, chord-extension overhangs of 0.075c and 0.15c (where c is the wing chord), leading-edge notches cut out at the inboard end of the 0.075c chord-extension to depths of 0.075c and 0.125c, and indentation of the model fuselage to conform partially to the supersonic area rule for a Mach number of 1.20. Lift, drag, and pitching-moment data were obtained for configurations with the tail on and off. Comparisons of data obtained from the present model with data from a configuration with leading-edge slats are included.
Aerodynamic Characteristics at Transonic Speeds of an Airplane Configuration with an 83.5 Deg Delta Wing Having Auxiliary Variable-sweep Wing Panels
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 230
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 230
Book Description
Preliminary Investigation of Subsonic and Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Airplane Configuration Having Externally Mounted Engines
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 108
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 108
Book Description
Subsonic Aerodynamic Characteristics of an Airplane Configuration Utilizing a Variable-sweep Wing Having a Free-floating Apex
Author: Edward Charles Polhamus
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description