Effect Of Longitudinal Wings Position On The Pressure Characteristics At Transonic Speeds Of A 45c Sweptback Wing Fuselage Model PDF Download
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Author | : William Solomon |
Publisher | : |
Total Pages | : 44 |
Release | : 1953 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Download Effect of Longitudinal Wings Position on the Pressure Characteristics at Transonic Speeds of a 45© Sweptback Wing-fuselage Model Book in PDF, ePub and Kindle
Author | : William Solomon |
Publisher | : |
Total Pages | : 36 |
Release | : 1953 |
Genre | : |
ISBN | : |
Download Effect of Longitudinal Wing Position on the Pressure Characteristics at Transonic Speeds of a 45 Degree Sweptback Wing-fuselage Model Book in PDF, ePub and Kindle
Author | : Joseph M. Hallissy |
Publisher | : |
Total Pages | : 38 |
Release | : 1953 |
Genre | : |
ISBN | : |
Download Transonic Characteristics of a 45 Degree Sweptback Wing-fuselage Combination Book in PDF, ePub and Kindle
Author | : Harold L. Robinson |
Publisher | : |
Total Pages | : 94 |
Release | : 1954 |
Genre | : Aerodynamic load |
ISBN | : |
Download The Effects of Wing Incidence on the Aerodynamic Loading Characteristics of a Sweptback Wing-body Combination at Transonic Speeds Book in PDF, ePub and Kindle
Author | : Earl D. Knechtel |
Publisher | : |
Total Pages | : 32 |
Release | : 1957 |
Genre | : Airplanes |
ISBN | : |
Download Effects of Wing-tip Droop on the Longitudinal Characteristics of Two Highly Swept Wing-body Combinations at Mach Numbers from 0.6 to 1.4 Book in PDF, ePub and Kindle
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stability characteristics of a 53 and a 63 degree sweptback wing-body combination. Both models were tested with flat and abruptly drooped wing tips. The 63 degree wing was also tested with a curved drooped tip. In addition, the combined effects of wing fences and extended leading-edge flaps were investigated. The results showed that abrupt droop of the outer 40 percent of the basic 53 degree wing improved the stability characteristics of the model. For the 63 degree swept wing, curved droop caused slight beneficial effects on the stability, whereas abrupt droop caused adverse effects. In general, the most favorable stability characteristics were obtained for either flat or abruptly drooped wings with fences and extended leading-edge flaps.
Author | : Albert G. Few |
Publisher | : |
Total Pages | : 80 |
Release | : 1954 |
Genre | : Airplanes |
ISBN | : |
Download Some Effects of Tail Height and Wing Plan Form on the Static Longitudinal Stability Characteristics of a Small-scale Model at High Subsonic Speeds Book in PDF, ePub and Kindle
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.
Author | : George L. Pratt |
Publisher | : |
Total Pages | : 110 |
Release | : 1952 |
Genre | : Airplanes |
ISBN | : |
Download Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations Book in PDF, ePub and Kindle
Author | : Jacob H. Lichtenstein |
Publisher | : |
Total Pages | : 34 |
Release | : 1951 |
Genre | : Airplanes |
ISBN | : |
Download Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces Book in PDF, ePub and Kindle
Wind-tunnel results are presented to show the effect of changes in horizontal-tail location on the low-speed static longitudinal stability and steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees.
Author | : Stanley H. Spooner |
Publisher | : |
Total Pages | : 28 |
Release | : 1956 |
Genre | : Aerodynamics, Transonic |
ISBN | : |
Download Combined Effects of Wing Taper and Low Horizontal-tail Position on Longitudinal Stability of a 45 Degree Sweptback Wing-body Combination at Transonic Speeds Book in PDF, ePub and Kindle
The combined effects of wing taper ratio and low horizontal-tail position on the static longitudinal stability of a 45 degree sweptback wing-body combination with an aspect ratio of approximately 4 have been investigated for a range of Mach numbers from 0.8 to 1.2 in the Langley 8-foot transonic pressure tunnel.
Author | : William B. Kemp |
Publisher | : |
Total Pages | : 32 |
Release | : 1953 |
Genre | : Airplanes |
ISBN | : |
Download Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35© Sweptback Wings Book in PDF, ePub and Kindle