Author: James Blaine ScarboroughPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28
Book Description
Some Problems on the Lift and Rolling Moment of Airplane Wings
Author: James Blaine ScarboroughPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28
Book Description
Some problems on the lift and rolling moment of airplane wings
Author: Some Problems on the Lift and Rolling Moment of Airplane Wings
Author: Elliott G. ReidPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
Book Description
Some Problems on the Lift and Rolling Moment of Airplane Wings, by James B. Scarborough, a Dissertation...
Author: James Blaine ScarboroughPublisher:
ISBN:
Category :
Languages : en
Pages : 17
Book Description
Influence of Large Amounts of Wing Sweep on Stability and Control Problems of Aircraft
Author: Hartley Akin SoulePublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42
Book Description
The use of large amounts of sweep has been suggested in this country and in Germany as a means of avoiding some of the drag increase and stability and control difficulties encountered in high-speed flight with conventional straight-wing airplanes. Experience with sweep in tailless airplanes and studies made since this suggested has been made have indicated that the use of a large amount of sweep will, in itself, introduce stability and control problems of sufficient magnitude and complexity to require considerable research, particularly for flight at high angles of attack. The paper discusses these problems and, although no proved solutions are given, in some cases promising lines for further investigation are presented.
Three-dimensional Unsteady Lift Problems in High-speed Flight
Author: Harvard LomaxPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 72
Book Description
The indicial lift and pitching-moment coefficients are derived for flat-plate triangular wings at supersonic speeds. Coefficients are determined for angle-of-attack distributions corresponding to sinking and pitching wings. The wing with supersonic edges is completely analyzed, the wing with subsonic edges is partially analyzed; the solution in this case being completed for very narrow wings by an application of slender wing theory. In case of the supersonic edges, a comparison is made with known two-dimensional results and also with results for the same triangular wing in reversed flow.
Some Problems on the Lift and Rolloing Moment on Airplane Wings
Author: James B.. ScarrboroughPublisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
Preliminary Investigation at Low Speeds of Swept Wings in Rolling Flow
Author: David FeigenbaumPublisher:
ISBN:
Category : Air flow
Languages : en
Pages : 36
Book Description
Glider Flying Handbook
Author: Federal Aviation AdministrationPublisher: Skyhorse Publishing Inc.
ISBN: 1602390614
Category : Education
Languages : en
Pages : 241
Book Description
For both certified glider pilots and students attempting certification in the glider category, this is an unparalleled...
The Rolling Moment Due to Sideslip of Swept Wings at Subsonic and Transonic Speeds
Author: Edward C. PolhamusPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 90
Book Description
A summary and analysis has been made of results obtained in a systematic research program concerned with the effects of wing sweep, aspect ratio, taper ratio, and dihedral on the rolling moment due to sideslip characteristics of wing-fuselage configurations up to Mach numbers of about 0.95. Other test results are presented to show trends of rolling moment due to sideslip with Mach number for a few wings in the transonic and supersonic speed range.