Download or read book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 449 Swept Wing written by and published by . This book was released on 1978 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44 Deg Swept Wing written by and published by . This book was released on 1978 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44 swept Wing written by William P. Henderson and published by . This book was released on 1978 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Wing Leading edge Flap Deflections on Subsonic Longitudinal Aerodynamic Characteristics of a Wing fuselage Configuration with a 44 S wept Wing written by William P. Henderson and published by . This book was released on 1978 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of wing leading edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing body configurations at subsonic speeds written by William P. Henderson and published by . This book was released on 1976 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Investigation of Effects of Wing Leading and Trailing edge Flap Deflections and Canard Incidence on a Fighter Configuration Equipped with a Forward swept Wing written by Thomas G. Gainer and published by . This book was released on 1984 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book High subsonic speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta wing Configurations for Angles of Attack from 0 to 90 written by Bernard Spencer and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Effects of Fuselage Size on the Low speed Longitudinal Aerodynamic Characteristics of a Thin 60 Delta Wing with and Without a Double Slotted Flap written by John M. Riebe and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low speed Investigation of the Effects of Wing Flap Deflection and Horizontal tail Configuration on the Longitudinal Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips written by William C. Jr Hayes and published by . This book was released on 1960 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Wing Leading edge Radius and Reynold Number on Longitudinal Aerodynamic Characteristics of Highly Swept Wing body Configurations at Subsonic Speeds written by William P. Henderson and published by . This book was released on 1976 with total page 53 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Experimental Investigation at High Subsonic Speeds of the Effects of Leading edge Radius on the Aerodynamic Characteristics of a Sweptback wing fuselage Combination with Leading edge Flaps and Chord extensions written by Kenneth P. Spreemann and published by . This book was released on 1955 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt: A limited investigation was made at high subsonic speeds to determine the effects of a wing leading-edge radius on the aerodynamic characteristics of a sweptback-wing-fuselage combination with leading-edge flaps and chord-extensions. The basic wing had 45 degree sweepback, aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section. The leading-edge shapes considered consisted of a sharp leading edge, a normal airfoil leading edge, and a leading edge formed by using three times the normal radius and fairing the new nose contour smoothly into the normal airfoil. The investigation was made in the Langley high-speed 7- by 10-foot tunnel over a Mach number range of 0.80 to 0.92 and an angle-of-attack range of -2 to 24 degrees. Lift, drag, and pitching-moment data were obtained for all configurations with leading-edge flap deflections of 0 to 6 degrees.

Download or read book Subsonic Aerodynamic Characteristics of a Highly Swept Fixed Wing Configuration with Variation in Wing Dihedral Angle written by William P. Henderson and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Wing transition Location and Slotted and Unslotted Flaps on Aerodynamic Characteristics of a Fighter Model at High Subsonic Speeds written by and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small scale Model at High Subsonic Speeds written by Albert G. Few and published by . This book was released on 1954 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: The drag due to lift increases with increasing sweep through the Mach number range. Some increase in bag due to lift is evident decrease in taper ratio for wings having 300of sweep through most of the speed range.

Download or read book Effects of Some Wing Variations Including Wingtip Deflection on the Static Longitudinal Aerodynamic Characteristics of a Delta wing Configuration at Supersonic Speeds written by and published by . This book was released on 1960 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Leading And Trailing Edge Flaps on Clipped Delta Wings with and Without Wing Camber at Supersonic Speeds written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of the aerodynamic characteristics of thin, moderately swept fighter wings has been conducted to evaluate the effect of camber and twist on the effectiveness of leading- and trailing-edge flaps at supersonic speeds in the Langley Unitary Plan Wind Tunnel. The study geometry consisted of a generic fuselage with camber typical of advanced fighter designs without inlets, canopy, or vertical tail. The model was tested with two wing configurations an uncambered (flat) wing and a cambered and twisted wing. Each wing had an identical clipped delta planform with an inboard leading edge swept back 65 deg and an outboard leading edge swept back 50 deg. The trailing edge was swept forward 25 deg. The leading-edge flaps were deflected 4 deg to 15 deg, and the trailing-edge flaps were deflected from -30 deg to 10 deg. Longitudinal force and moment data were obtained at Mach numbers of 1.60, 1.80, 2.00, and 2.16 for an angle-of-attack range 4 deg to 20 deg at a Reynolds number of 2.16 x 10(exp 6) per foot and for an angle-of-attack range 4 deg to 20 deg at a Reynolds number of 2.0 x 10(exp 6) per foot. Vapor screen, tuft, and oil flow visualization data are also included. Hernandez, Gloria and Wood, Richard M. and Covell, Peter F. Langley Research Center RESEARCH; INVESTIGATION; DESIGN; EXPLORATION...

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1975 with total page 970 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.