Aerodynamic Loading Characteristics In Sideslip Of A 45c Sweptback Wing With And Without A Fence At High Subsonic Speeds PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Aerodynamic Loading Characteristics In Sideslip Of A 45c Sweptback Wing With And Without A Fence At High Subsonic Speeds PDF full book. Access full book title Aerodynamic Loading Characteristics In Sideslip Of A 45c Sweptback Wing With And Without A Fence At High Subsonic Speeds.
Author | : Richard E. Kuhn |
Publisher | : |
Total Pages | : 50 |
Release | : 1955 |
Genre | : Aerodynamic load |
ISBN | : |
Download Aerodynamic Loading Characteristics in Sideslip of a 45© Sweptback Wing with and Without a Fence at High Subsonic Speeds Book in PDF, ePub and Kindle
Author | : M. Leroy Spearman |
Publisher | : |
Total Pages | : 34 |
Release | : 1957 |
Genre | : Airplanes |
ISBN | : |
Download Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45© Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail Book in PDF, ePub and Kindle
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.
Author | : James W. Wiggins |
Publisher | : |
Total Pages | : 32 |
Release | : 1954 |
Genre | : Aerodynamic load |
ISBN | : |
Download Wind-tunnel Investigation of the Effects of Steady Rolling on the Aerodynamic Loading Characteristics of a 45© Sweptback Wing at High Subsonic Speeds Book in PDF, ePub and Kindle
Author | : Paul G. Fournier |
Publisher | : |
Total Pages | : 34 |
Release | : 1953 |
Genre | : Airplanes |
ISBN | : |
Download Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch and Sideslip at High Subsonic Speeds of a Wing-fuselage Combination Having a Triangular Wing of Aspect Ratio 4 Book in PDF, ePub and Kindle
The results presented in the present paper are part of a program conducted to investigate the effect of wing plan form on the aerodynamic characteristics in pitch, in sideslip, and during steady roll. This paper presents the aerodynamic characteristics in pitch and sideslip at high subsonic speeds of a wing-fuselage combination having a triangular wing of aspect ratio 4, a leading-edge sweep of angle of 45 degrees, and with an NACA 65A006 airfoil section parallel to the plane of symmetry.
Author | : Douglas R. Lord |
Publisher | : |
Total Pages | : 52 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : |
Download Aerodynamic Characteristics of a Spoiler-slot-deflector Control on a 45© Sweptback Wing at Mach Numbers of 1.61 and 2.01 Book in PDF, ePub and Kindle
An investigation has been made in the Langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.61 and 2.01 to determine the aerodynamic characteristics of a spoiler-slot-deflector control on a 45 degree sweptback wing having an aspect ratio of 3.5, a taper ratio of 0.3, and an NACA 65A005 airfoil section. The model was equipped with a 15-percent-chord spoiler-slot-deflector extending from 13 o 78 percent of the wing semispan. The spoiler and deflector were hinged along the 60- and 75-percent-chord lines, respectively. Tests were made at a Reynolds number of 3,000,000 (based on the mean aerodynamic chord of the wing) and covered ranges of angles of attack from -3 to 15 degrees, spoiler projections from 0 to 8.0 percent chord, and deflector projections from 0 to 7.6 percent chord.
Author | : Donald D. Arabian |
Publisher | : |
Total Pages | : 54 |
Release | : 1954 |
Genre | : Airplanes |
ISBN | : |
Download Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45© Sweptback Wing at Transonic Speeds Book in PDF, ePub and Kindle
Author | : Donald D. Arabian |
Publisher | : |
Total Pages | : 54 |
Release | : 1961 |
Genre | : Airplanes |
ISBN | : |
Download Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45 Degree Sweptback Wing at Transonic Speeds Book in PDF, ePub and Kindle
Author | : Atwood R. Heath |
Publisher | : |
Total Pages | : 92 |
Release | : 1960 |
Genre | : Mach number |
ISBN | : |
Download Longitudinal Aerodynamic Characteristics of a High-subsonic-speed Transport Airplane Model with a Cambered 40° Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0.96 Book in PDF, ePub and Kindle
Author | : Edward C. Polhamus |
Publisher | : |
Total Pages | : 36 |
Release | : 1958 |
Genre | : Airplanes |
ISBN | : |
Download Effect at High Subsonic Speeds of Fuselage Forebody Strakes on the Static Stability and Vertical-tail-load Characteristics of a Complete Model Having a Delta Wing Book in PDF, ePub and Kindle
A wind-tunnel investigation at high subsonic speeds has been conducted to determine the effect of fuselage forebody strakes on the static stability and the vertical-tail-load characteristics of an airplane-type configuration having a delta wing. The tests were made at Mach numbers from 0.60 to 0.92 corresponding to Reynolds numbers from 3,000,000 to 4,200,000, based on the wing mean aerodynamic chord, and at angles of attack from approximately -2 to 24 degrees.
Author | : John DeYoung |
Publisher | : |
Total Pages | : 106 |
Release | : 1950 |
Genre | : Aerodynamic load |
ISBN | : |
Download Theoretical Antisymmetric Span Loading for Wings of Arbitrary Plan Form at Subsonic Speeds Book in PDF, ePub and Kindle
A simplified lifting-surface theory that includes effects of compressibility and spanwise variation of section lift-curve slope is used to provide charts with which antisymmetric loading due to arbitrary antisymmetric angle of attack can be found for wings having symmetric plan forms with a constant spanwise sweep angle of the quarter-chord line. Consideration is given to the flexible wing in roll. Aerodynamic characteristics due to rolling, deflected ailerons, and sideslip of wings with dihedral are considered. Solutions are presented for straight-tapered wings for a range of swept plan forms.