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:
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.
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.
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:
Download or read book Journal of Aircraft written by and published by . This book was released on 1972 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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:
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.
Download or read book A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4 0 X 10 6 written by William C. Schneider and published by . This book was released on 1952 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45 Degree Sweptback Wing of Aspect Ratio 8 02 at a Reynolds Number of 4 0 X 10 6 written by William C. Schneider and published by . This book was released on 1954 with total page 9 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low speed Characteristics of a 45 Degrees Sweptback Wing of Aspect Ratio 8 from Pressure Distributions and Force Tests at Reynolds Numbers from 1 500 000 to 4 800 000 written by Robert R. Graham and published by . This book was released on 1951 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Comparison of the Spanwise Loading Calculated by Various Methods with Experimental Loadings Obtained on a 45 degree Sweptback Wing of Aspect Ratio 8 02 at a Reynolds Number 4 0 X 106 written by William C. Schneider and published by . This book was released on 1954 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Loading Characteristics in Sideslip of a 45 Sweptback Wing with and Without a Fence at High Subsonic Speeds written by Richard E. Kuhn and published by . This book was released on 1955 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Low speed Lift and Pitching moment Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 with and Without High lift and Stall control Devices as Determined from Pressure Distributions at a Reynolds Number of 4 0 X 10 6 written by Thomas V. Bollech and published by . This book was released on 1953 with total page 55 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Twist and Camber Fences and Horizontal tail Height on the Low speed Longitudinal Stability Characteristcs of a Wing fuselage Combination with a 45 Degree Sweptback Wing of Aspect Ratio 8 at a Reynolds Number of 4 0 X 10 6 written by Gerald V. Foster and published by . This book was released on 1952 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
