Author : United States. Civil Aeronautics Board
Publisher :
Page : 278 pages
File Size : 15,72 MB
Release :
Category :
ISBN :
Author :
Publisher :
Page : 502 pages
File Size : 28,13 MB
Release : 1948
Category :
ISBN :
Author : United States. Civil Aeronautics Board
Publisher :
Page : 454 pages
File Size : 17,80 MB
Release : 1949
Category : Aeronautics, Commercial
ISBN :
Author : United States. Superintendent of Documents
Publisher :
Page : 1714 pages
File Size : 12,50 MB
Release : 1959
Category : Government publications
ISBN :
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
Author : United States. Congress. Senate. Committee on Commerce. Aviation Subcommittee
Publisher :
Page : 1340 pages
File Size : 27,3 MB
Release : 1976
Category : Aeronautics
ISBN :
Author : William A. Jordan
Publisher : Praeger
Page : 380 pages
File Size : 19,48 MB
Release : 1979
Category : Business & Economics
ISBN :
Get the real, full TAB for 16 fierce metal guitar onslaughts. Titles: All I Want (Staind) * Away From Me (Puddle of Mudd) * Believe (Staind) * * Blurry (Puddle of Mudd) * Breakdown (Seether) * Broken (Seether) * Fake It (Seether) * Indestructible (Disturbed) * Inside the Fire (Disturbed) * Livin’ on Borrowed Time (Puddle of Mudd) * Perfect Insanity (Disturbed) * Psycho (Puddle of Mudd) * Right Here(Staind) * Rise Above This (Seether) * So Far Away (Staind) * Ten Thousand Fists (Disturbed).
Author : United States. Congress. Senate. Committee on Commerce
Publisher :
Page : 2322 pages
File Size : 28,5 MB
Release : 1976
Category : Railroad law
ISBN :
Author : United States. Congress. Senate. Committee on Commerce
Publisher :
Page : 1370 pages
File Size : 32,23 MB
Release : 1976
Category : Legislative hearings
ISBN :
Author :
Publisher :
Page : 468 pages
File Size : 24,73 MB
Release : 1956
Category : Aeronautics
ISBN :
Author : Kenneth P. Spreemann
Publisher :
Page : 644 pages
File Size : 34,28 MB
Release : 1957
Category : Airplanes
ISBN :
This investigation was made to determine the effects of 6 degree full-span and 3 degree partial-span leading-edge flaps in combination with chord-extensions or fences on the aerodynamic characteristics of a wing-fuselage configuration with a 45 degree sweptback wing of aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil sections. The investigation was made in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.40 to 0.93 and an angle-of-attack range of about -2 degrees to 24 degrees. Lift, drag, and pitching-moment data were obtained for all configurations. From overall considerations of stability and performance it appears that with the model of this investigation the 6 degree full-span leading-edge flaps in combination with the chord-extension over the outboard 35 percent of the span, with or without leading-edge camber, would be the most desirable configuration.
