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The Lift Distribution Of Swept Back Wings
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Book Synopsis The Lift Distribution of Swept-back Wings by : United States. Air Force. Air Matériel Command
Download or read book The Lift Distribution of Swept-back Wings written by United States. Air Force. Air Matériel Command and published by . This book was released on 1946 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two procedures for calculating the lift distribution along the span are given, in which better account is taken of the distribution of circulation over the area than in the Prandtl lifting-line theory. The methods are also applicable to wings with sweepback. Calculated results according to two methods agree excellently. Using the second, simpler method one needs about 3 hours for the calculation of the lift distribution of a straight wing, and about eight hours for this calculation for the swept-back wing. The results are compared with those of the Multhopp method and with experimental results. Finally there is a brief not on the swept-back wing in sideslip.
Book Synopsis The Lift Distribution of Swept-back Wings by : J. Weissinger
Download or read book The Lift Distribution of Swept-back Wings written by J. Weissinger and published by . This book was released on 1982 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Note on the Calculation of the Lift Distribution of Swept Wings by : H. Schlichting
Download or read book Note on the Calculation of the Lift Distribution of Swept Wings written by H. Schlichting and published by . This book was released on 1947 with total page 131 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Swept-back Wings with Arbitrary Lift Distribution by : Feodor Theilheimer
Download or read book Swept-back Wings with Arbitrary Lift Distribution written by Feodor Theilheimer and published by . This book was released on 1942 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Theoretical Distribution of Load Over a Swept-back Wing by : Doris Cohen
Download or read book Theoretical Distribution of Load Over a Swept-back Wing written by Doris Cohen and published by . This book was released on 1942 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt: The load over an elliptical wing with 30 degrees sweepback has been calculated by a method, based on vortex theory, which takes account of the chordwise distribution of lifting area. The theory indicates a 14-percent loss in total lift due to the introduction of sweepback, with the greatest loss taking place at the center of the span. An increase in concentration of load at the tips is also indicated. The results are compared with the results previously obtained by somewhat simpler calculations based on the assumption of a single lifting vortex.
Book Synopsis Pressure Distribution Measurements of Swept-back Wings (Second Report on Swept-back Wings) by : H. Luetgebrune
Download or read book Pressure Distribution Measurements of Swept-back Wings (Second Report on Swept-back Wings) written by H. Luetgebrune and published by . This book was released on 1946 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure distribution measurements were carried out on a straight wing, a strongly swept-back wing, and on a strongly swept forward wing. The experimental results were compared with Multhopp's theoretical lift distribution.
Book Synopsis Calculation of Lift Distribution of Swept Wings by : H. Schlichting
Download or read book Calculation of Lift Distribution of Swept Wings written by H. Schlichting and published by . This book was released on 1948 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms by : Harvard Lomax
Download or read book Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms written by Harvard Lomax and published by . This book was released on 1949 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.
Book Synopsis The Spanwise Lift Distribution of Swept Wings at Subsonic Speeds by : Eli Herman Benstein
Download or read book The Spanwise Lift Distribution of Swept Wings at Subsonic Speeds written by Eli Herman Benstein and published by . This book was released on 1952 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Lift Distribution on Swept - Back Wings in Yaw by : Luckert. H.J.
Download or read book Lift Distribution on Swept - Back Wings in Yaw written by Luckert. H.J. and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Calculated Lift Distribution in Incompressible Flow on Some Sweptback Wings by : J. A. Bagley
Download or read book Calculated Lift Distribution in Incompressible Flow on Some Sweptback Wings written by J. A. Bagley and published by . This book was released on 1962 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Simple Method of Estimating the Subsonic Lift and Damping in Roll of Sweptback Wings by : Edward C. Polhamus
Download or read book A Simple Method of Estimating the Subsonic Lift and Damping in Roll of Sweptback Wings written by Edward C. Polhamus and published by . This book was released on 1949 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method of modifying existing correction factors of lifting-surface theory to account approximately for the effects of sweep has been derived, and these factors have been applied to existing lifting-line theories for the lift and damping in roll of swept wings. A comparison with experimental data in the low-speed and low lift range indicated good agreement for wings of any plan form. If the Glauert-Prandtl transformation is used, the formulas obtained can be applied to swept wings at subsonic speeds below the critical speed.
Book Synopsis Wind-tunnel Lift Interference on Sweptback Wings in Rectangular Test Sections with Slotted Top and Bottom Walls by : Ray H. Wright
Download or read book Wind-tunnel Lift Interference on Sweptback Wings in Rectangular Test Sections with Slotted Top and Bottom Walls written by Ray H. Wright and published by . This book was released on 1966 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Review of the Stall Characteristics of Swept Wings by : Charles W. Harper (Jr.)
Download or read book A Review of the Stall Characteristics of Swept Wings written by Charles W. Harper (Jr.) and published by . This book was released on 1964 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment by : Robert T. Jones
Download or read book The Spanwise Distribution of Lift for Minimum Induced Drag of Wings Having a Given Lift and a Given Bending Moment written by Robert T. Jones and published by . This book was released on 1950 with total page 708 pages. Available in PDF, EPUB and Kindle. Book excerpt: The problem of the minimum induced drag of wings having a given lift and a given span is extended to include cases in which the bending moment to be supported by the wing is also given. Expressions for the spanwise load distribution and the minimum drag in terms of the lateral position of the load centroid are given. The results show a 15-percent reduction of the induced drag with a 15-percent increase in span over that for an elliptic loading having the same total lift and bending moment.
Book Synopsis Rolling and Yawing Moments for Swept-back Wings in Sideslip at Supersonic Sppeds by : Seymour Lampert
Download or read book Rolling and Yawing Moments for Swept-back Wings in Sideslip at Supersonic Sppeds written by Seymour Lampert and published by . This book was released on 1951 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is presented for determining the rolling and yawing moments of swept-back wings in steady sideslip at supersonic speeds. The case treated in particular is that of a swept tapered wing with all edges subsonic.
Book Synopsis Wind-tunnel Lift Interference on Sweptback Wings in Rectangular Test Sections with Slotted Side Walls by : Ray H. Wright
Download or read book Wind-tunnel Lift Interference on Sweptback Wings in Rectangular Test Sections with Slotted Side Walls written by Ray H. Wright and published by . This book was released on 1970 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theory is presented for the boundary-induced upwash interference on a sweptback wing mounted in a rectangular wind-tunnel test section with closed top and bottom walls and slotted side walls. The interference factor can be computed at any point in the test section. In an example, the interference with slotted side walls is compared with that with slotted top and bottom walls.
