Author: Publisher:
ISBN:
Category :
Languages : en
Pages : 428
Book Description
Reynolds Number Effects on the Aerodynamic Characteristics of Irregular Planform Wings at Mach Number 0.3
Author: Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63
Author: Maurice O. FerynEffects at Mach Numbers of 1.61 and 2.01 of Camber and Twist on the Aerodynamic Characteristics of Three Swept Wings Having the Same Planform
Author: Emma Jean LandrumPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52
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
The Effects of Mach Number and Reynolds Number on the Aerodynamic Characteristics of Several 12-percent-thick Wings Having 35 Degrees of Sweepback and Various Amounts of Camber
Author: Bruce E. TinlingPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 68
Book Description
A comparison of the lift, drag, and pitching-moment characteristics of several wings having 35 degrees of sweepback and various amounts and various amounts of camber has been made from the results of wind-tunnel tests. Six semispan model wings were tested: three having an aspect ratio of 10, and three having an aspect ratio of 5. The streamwise sections for the three wings of each aspect ratio were the NACA 65(1)A012, the NACA 64(1)A312, and the NACA 64(1)A612. The Reynolds number was varied from 2,000,000 to 10,000,000 at a Mach number of 0.25, and the Mach number was varied from 0.25 to 0.92 at a Reynolds number of 2,000,000.
Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94
Author: Edward J. HopkinsPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
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: Jr. John E. Hatch