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The Interference Effects Of A Body On The Spanwise Load Distributions Of Two 45 Sweptback Wings Of Aspect Ratio 802 From Low Speed Tests
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Book Synopsis The Interference Effects of a Body on the Spanwise Load Distributions of Two 45° Sweptback Wings of Aspect Ratio 8.02 from Low-speed Tests by : Albert P. Martina
Download or read book The Interference Effects of a Body on the Spanwise Load Distributions of Two 45° Sweptback Wings of Aspect Ratio 8.02 from Low-speed Tests written by Albert P. Martina and published by . This book was released on 1956 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degrees Sweptback Wings of Aspect Ratio 8 from Low-speed Tests at a Reynolds Number of 4 X (10)6 by : Albert P. Martina
Download or read book The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degrees Sweptback Wings of Aspect Ratio 8 from Low-speed Tests at a Reynolds Number of 4 X (10)6 written by Albert P. Martina and published by . This book was released on 1952 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degree Sweptback Wings of Aspect Ratio 8.02 from Low-speed Tests by : Albert P. Martina
Download or read book The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degree Sweptback Wings of Aspect Ratio 8.02 from Low-speed Tests written by Albert P. Martina and published by . This book was released on 1956 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: The addition of the body to the plane wing increased the exposed wing loading at a given lift coefficient as much as 10 percent with the body at 0 degrees incidence and 4 percent at 4 degrees incidence. The bending-moment coefficients at the wing-body juncture were increased about 2 percent with the body at 0 degrees incidence, whereas the increases were as much as 10 percent with the body at 4 degrees incidence.
Book Synopsis The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degree Sweptback Wings of Aspect Ratio 8 from Low-speed Tests at a Reynolds Number of 4,000,000 by : Albert B. Martina
Download or read book The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degree Sweptback Wings of Aspect Ratio 8 from Low-speed Tests at a Reynolds Number of 4,000,000 written by Albert B. Martina and published by . This book was released on 1952 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests of two wing-body combinations have been conducted in the Langley 19-foot pressure tunnel at a Reynolds number of 4,000,000 and a Mach number of 0.19 to determine the effects of the bodies on the wing span load distributions. The wings had 4 5° sweepback of the quarter-chord line, aspect ratio 8.02, taper ratio 0.45, and incorporated 12-percent-thick airfoil sections streamwise. One wing was untwisted and uncambered whereas the second wing incorporated both twist and camber. Identical bodies of revolution, of 10:1 fineness ratio, having diameter-to-span ratios of 0.10, were mounted in mid -high-wing arrangements. The effects of wing incidence, wing fences, and flap deflection were determined for the plane uncambered wing.
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1977 with total page 1006 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing by : Donald E. Hewes
Download or read book The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing written by Donald E. Hewes and published by . This book was released on 1951 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.
Book Synopsis Effects of Twist and Camber on the Low-speed Characteristics of a Large-scale 45 Degree Swept-back Wing by : Lynn W. Hunton
Download or read book Effects of Twist and Camber on the Low-speed Characteristics of a Large-scale 45 Degree Swept-back Wing written by Lynn W. Hunton and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Calculation of Span Load Distributions on Swept-back Wings by : William Mutterperl
Download or read book The Calculation of Span Load Distributions on Swept-back Wings written by William Mutterperl and published by . This book was released on 1941 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Span load distributions of swept-back wings have been calculated. The method used was to replace the wing with a bound vortex at the quarter-chord line and to calculate the downwash due to the system of bound and trailing vortices to conform at the three-quarter-chord line to the slope of the flat-plate wing surface. Results are given for constant-chord and 5:1 tapered plan forms, for swee-pback angles of 0, 30 and 45 degresss, and for aspect ratios of 3, 6, and 9. Some comments on the stalling of swept-back wings are included.
Download or read book Spanwise Air-load Distribution written by and published by . This book was released on 1938 with total page 238 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10(exp 6) to 4.8 X 10(exp 6) as Determined by Pressure Distributions, Force Tests by : George L. Pratt
Download or read book Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10(exp 6) to 4.8 X 10(exp 6) as Determined by Pressure Distributions, Force Tests written by George L. Pratt and published by . This book was released on 1952 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Linear Spanwise Variations of Twist and Circular-arc Camber on Low-speed Static Stability, Rolling, and Yawing Characteristics of a 45 [degrees] Sweptback Wing of Aspect Ratio 4 and Taper Ratio 0.6 by : Byron M. Jaquet
Download or read book Effect of Linear Spanwise Variations of Twist and Circular-arc Camber on Low-speed Static Stability, Rolling, and Yawing Characteristics of a 45 [degrees] Sweptback Wing of Aspect Ratio 4 and Taper Ratio 0.6 written by Byron M. Jaquet and published by . This book was released on 1952 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 O Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10 6 to 4.8 X 10 6 as Determined by Pressure Distributions, Force Tests, and Calculations by : George L. Pratt
Download or read book Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 O Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10 6 to 4.8 X 10 6 as Determined by Pressure Distributions, Force Tests, and Calculations written by George L. Pratt and published by . This book was released on 1952 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X (10)6 to 4.8 X (10)6 as Determined by Pressure Distributions, Force Tests, and Calculations by : George L. Pratt
Download or read book Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X (10)6 to 4.8 X (10)6 as Determined by Pressure Distributions, Force Tests, and Calculations written by George L. Pratt and published by . This book was released on 1952 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effect of Linear Spanwise Variations of Twist and Circular-Arc Camber on Low-Speed Static Stability, Rolling, and Yawing Characteristics of a 45 Degrees Sweptback Wing of Aspect Ratio 4 and Taper Ration 0.6 by :
Download or read book Effect of Linear Spanwise Variations of Twist and Circular-Arc Camber on Low-Speed Static Stability, Rolling, and Yawing Characteristics of a 45 Degrees Sweptback Wing of Aspect Ratio 4 and Taper Ration 0.6 written by and published by . This book was released on 1952 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation at low scale has been made in the Langley stab unity tunnel in order to determine the effect of linear spanwise variations of twist and circular-arc camber on the low-speed aerodynamic characteristics and static-stability and rotary-stability (rolling and yawing) derivatives of a wing of aspect ratio 4, taper ratio 0.6, and with 45 deg sweepback of the quarter-chord line. Results of the investigation indicate that twist or camber produced only small changes in the maximum lift coefficient. A combination of camber and twist was more effective than twist alone in providing an increase in the maximum lift-to-drag ratio in the moderate lift-coefficient range for the wings investigated. The variation of static longitudinal stability through the lift-coefficient range was less for the twisted wing than for the twisted and cambered or plane wing. A combination of twist and camber generally extended the initial linear range of several of the static- and rotary-stability derivatives to a higher lift coefficient and, although these effects were small, higher Reynolds numbers may result in larger effects.
Book Synopsis Low-Speed Tests on 45-deg Swept-Back Wings. Part I. Pressure Measurements on Wings of Aspect Ratio 5. Part II. Balance and Pressure Measurements on Wings of Different Aspect Ratios by : J. Weber
Download or read book Low-Speed Tests on 45-deg Swept-Back Wings. Part I. Pressure Measurements on Wings of Aspect Ratio 5. Part II. Balance and Pressure Measurements on Wings of Different Aspect Ratios written by J. Weber and published by . This book was released on 1951 with total page 91 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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