Static Aerodynamic Characteristics Of A Model Of A Typical Subsonic Jet Transport Airplane At Mach Numbers From 040 To 120 PDF Download
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Author | : Eugene N. Brooks |
Publisher | : |
Total Pages | : 44 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet-transport Airplane at Mach Numbers from 0.40 to 1.20 Book in PDF, ePub and Kindle
Author | : Howard F. Savage |
Publisher | : |
Total Pages | : 662 |
Release | : 1957 |
Genre | : Aerodynamics |
ISBN | : |
Download The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3 Book in PDF, ePub and Kindle
An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.
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 | : |
Publisher | : |
Total Pages | : 96 |
Release | : 1960 |
Genre | : |
ISBN | : |
Download Longitudinal Aerodynamic Characteristics of a High-subsonic-speed Transport Airplane Model with a Cambered 40 Deg Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0.96 Book in PDF, ePub and Kindle
Author | : Kenneth W. Goodson |
Publisher | : |
Total Pages | : 64 |
Release | : 1961 |
Genre | : Stability of airplanes, Longitudinal |
ISBN | : |
Download Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configurations Book in PDF, ePub and Kindle
An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00 wing had a zero taper and an unswept 0.80 chord line. Several aspect-ratio modifications to the basic wing were made by clipping off portions of the wing tips. The complete model was tested with a chord-plane tail, a T-tail, and a biplane tail (combined T-tail and chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92. The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the biplane tail giving the best overall characteristics as regards pitching-moment linearity. Changes in static margin at zero lift coefficient with Mach number were small for the model with these tails over the Mach number range investigated.
Author | : Edward J. Ray |
Publisher | : |
Total Pages | : 88 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Longitudinal Aerodynamic Characteristics at Mach Numbers from 0.50 to 1.19 of a Supersonic Transport Model with a Modified M Wing Book in PDF, ePub and Kindle
Author | : Kenneth W. Goodson |
Publisher | : |
Total Pages | : 102 |
Release | : 1961 |
Genre | : Stability of airplanes, Lateral |
ISBN | : |
Download Static Lateral Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configuration Book in PDF, ePub and Kindle
An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The aspect-ratio-3.50 wing had a taper of 0.067 and an unswept 0.80 chord line. The complete model was tested with a wing-chord-plane tail, a T-tail, and a biplane tail (combined T-tail and wing-chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92 over a range of angle of attack of about ±20° and a range of sideslip of -15° to 13°. Some data were obtained with the horizontal stabilizer deflected. A few tests were also made with the wing tips clipped to an aspect ratio of 3.00.
Author | : Paul G. Fournier |
Publisher | : |
Total Pages | : 72 |
Release | : 1961 |
Genre | : Aerodynamic load |
ISBN | : |
Download Aerodynamic Characteristics of a Canard and an Outboard-tail Airplane Model at High Subsonic Speeds Book in PDF, ePub and Kindle
Author | : Atwood R. Heath |
Publisher | : |
Total Pages | : 88 |
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 | : James C. Ferris |
Publisher | : |
Total Pages | : 66 |
Release | : 1966 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Download Transonic Aerodynamic Characteristics of a Model of a Supersonic Fighter-bomber Airplane with External Fuel Tanks and Other Modifications Book in PDF, ePub and Kindle