Author: Edward J. RayPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
Book Description
Effect of Wing Planform Modification on Longitudinal Characteristics of a Variable-sweep M Wing
Author: Edward J. RayPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
Book Description
Effect of Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable-sweep Wing Having an M Planform
Author: William P. HendersonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
Book Description
Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87
Author: Royce L. McKinneyPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
Book Description
Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels
Author: M. Leroy SpearmanPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36
Book Description
Effect of Wing Pivot Location on Longitudinal Aerodynamic Characteristics of a Variable Sweep Wing Having an M Planform
Author: Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-wing Airplane Model
Author: Charles L. SeacordPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 30
Book Description
Summary: An investigation of the power-off longitudinal stability characteristics of a tailless all-wing airplane model with various wing modifications has been made in the Langley free-flight tunnel. Force and tuft tests were made on the model in the original condition, with the wing tips rotated for washout, with rectangular and swept-forward tips, and with various slat arrangements. Flight tests were made with the original wing and with the original wing equipped with the most promising modifications. The results indicated that changes in tip plan form or rotation of the wing tips did not appreciably reduce the instability at high lift coefficients. Addition of wing slats, however, improved the longitudinal stability at the stall when the slat extended far enough inboard to cover the area that tended to stall first.
Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers from 1.70 to 4.63
Author: Lloyd S. JernellPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 74
Book Description
Author: 
Author: 
Author: Maurice O. Feryn