Author: Alexander H. FlaxPublisher:
ISBN:
Category :
Languages : en
Pages : 82
Book Description
The Aerodynamics of Low-aspect-ratio Wings and Wing-body Combinations
Author: Alexander H. FlaxAerodynamic-center Considerations of Wings and Wing-body Combinations
Author: John E. LamarThe Unsteady Aerodynamic Forces on Deforming, Low Aspect Ratio Wings and Slender Wing-body Combinations Oscillating Harmonically in a Compressible Flow, by R.D. Milne
Author: Ronald D. MilnePublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 42
Book Description
Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground
Author: Marvin P. FinkInvestigation of Some Effects of Flexibility on the Lift and Pitching-moment Characteristics of a Series of Low-aspect- Ratio Wing-body Combinations at Transonic Speeds
Author: Robert V. DoggettPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 58
Book Description
The Unsteady Aerodynamic Forces on Deforming, Low Aspect Ratio Wings and Slender Wing-body Combinations
Author: R. D. MilneLift, Drag, and Pitching Moment of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds
Author: John C. HeitmeyerPublisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 30
Book Description
Comments on the Aerodynamics of Low Aspect Ratio Wing-body-tail Combinations in Steady Supersonic Flow
Author: G. V. BullPublisher:
ISBN:
Category : Stability of airplanes
Languages : en
Pages : 37
Book Description
Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body
Author: John R. SevierPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44
Book Description
An Investigation at Transonic Speeds of the Effects of Thickness Ratio and of Thickened Root Sections on the Aerodynamic Characteristics of Wings with 47© Sweepback, Aspect Ratio 3.5, and Taper Ratio 0.2 in the Slotted Test Section of the Langley 8-foot High-speed Tunnel
Author: Ralph P. BielatPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 44
Book Description
Four wing-body combinations of the same plan form (47 degree sweep, 3.5 aspect ratio, and 0.2 taper ratio) were compared at transonic speeds in the Langley 8-foot high-speed tunnel. Three wings were 4, 6, and 9 percent thick; the fourth was 6 percent thick but, on the inner 0.4 span, tapered to 12-percent thickness at the roots.