Author: Williams J. AlfordPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 30
Book Description
An Exploratory Investigation of the Low-speed Aerodynamic Characteristics of Variable-wing-sweep Airplane Configurations
Author: Williams J. AlfordPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 30
Book Description
An Exploratory Investigation of the Low-speed Aerodynamic Characteristics of Variable-wing-sweep Airplane Configurations
Author: Williams J. AlfordPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 24
Book Description
An Exploratory Investigation of the Low-speed Aerodynamic Characteristics of Variable-wing- Sweep Airplane Configurations
Author: Investigation of the Low-speed Aerodynamic Characteristics of a Variable-sweep Airplane Model with a Twisted and Cambered Wing
Author: William B. Jr KempThe Transonic Aerodynamic Characteristics of Two Variable-sweep Airplane Configurations Capable of Low-level Supersonic Attack
Author: Ralph P. BielatPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 56
Book Description
Investigation of the Low-speed Aerodynamic Characteristics of a Variable-sweep Airplane Model with a Wing Having Partial-span Cambered-leading-edge Modifications
Author: Robert E. BechtLow-speed Investigation of the Effects of Wing Sweep on the Aerodynamic Characteristics of Parawings Having Equal-length Leading Edges and Keel
Author: Rodger L. NaesethPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 88
Book Description
An investigation has been made in the Langley 300-MPH 7- by 10-foot tunnel to determine the aerodynamic characteristics of a related series of parawings in which wing sweep was the primary variable. The leading-edge sweep angles varied from 400 to 750 and the three basic parawings had flat-planform sweep angles of 350, 450, and 550. The canopies of the wings were made of fabric. Tests were made at an airspeed of 38.6 mph and a Reynolds number of approximately 1.5 X 106. The maximum angle-of-attack range was from 140 to 530 for the wings having a canopy of 350 flat-planform sweep. A limited investigation of lateral characteristics was made for sideslip angles from approximately -50 to 160 for two angles of attack, and lateral stability derivatives were obtained for some configurations through a angle-of-attack range. Forces and moments acting on the wing and apex hinge moments were measured.
Subsonic Aerodynamic Characteristics of an Airplane Configuration Utilizing a Variable-sweep Wing Having a Free-floating Apex
Author: Edward Charles PolhamusPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings
Author: Bernard SpencerPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 98
Book Description
Author: