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Application Of The Leading Edge Suction Analogy To Prediction Of Longitudinal Load Distribution And Pitching Moments For Sharp Edged Delta Wings
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Book Synopsis Application of the Leading-edge-suction Analogy to Prediction of Longitudinal Load Distribution and Pitching Moments for Sharp-edged Delta Wings by : Melvin H. Snyder
Download or read book Application of the Leading-edge-suction Analogy to Prediction of Longitudinal Load Distribution and Pitching Moments for Sharp-edged Delta Wings written by Melvin H. Snyder and published by . This book was released on 1972 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The leading-edge-suction analogy of Polhamus has been used to develop the longitudinal load distribution of the vortex lift for delta wings. This distribution is shown to be similar in shape to that of the potential-flow longitudinal loading for delta wings having aspect ratios of 2 or less. The totals of the two theoretical distributions for delta wings with an aspect ratio near 1 are in good agreement with the experimentally determined loadings over the angle-of-attack range from 0 to 30 deg. The corresponding predicted pitching moments show slightly more stability than those measured, because of loss of lift near the wing tips.
Download or read book NASA Technical Note written by and published by . This book was released on 1973 with total page 478 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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 1972 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Book Synopsis Extension of Leading-edge-suction Analogy to Wings with Separated Flow Around the Side Edges at Subsonic Speeds by : John E. Lamar
Download or read book Extension of Leading-edge-suction Analogy to Wings with Separated Flow Around the Side Edges at Subsonic Speeds written by John E. Lamar and published by . This book was released on 1974 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper presents a method for determining the lift, drag, and pitching moment for wings which have separated flow at the leading and side edges with subsequently reattached flow downstream and inboard. Limiting values of the contribution to lift of the side-edge reattached flow are determined for rectangular wings. The general behavior of this contribution is computed for rectangular, cropped-delta, cropped-diamond, and cropped-arrow wings. Comparisons of the results of the method and experiment indicate reasonably good correlation of the lift, drag, and pitching moment for a wide planform range. The agreement of the method with experiment was as good as, or better than, that obtained by other methods. The procedure is computerized and is available from COSMIC as NASA Langley computer program A0313.
Book Synopsis Some Recent Applications of the Suction Analogy to Vortex-lift Estimates by :
Download or read book Some Recent Applications of the Suction Analogy to Vortex-lift Estimates written by and published by . This book was released on 1976 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Prediction of Lift and Drag for Slender Sharp-edge Delta Wings in Ground Proximity by : Charles H. Fox
Download or read book Prediction of Lift and Drag for Slender Sharp-edge Delta Wings in Ground Proximity written by Charles H. Fox and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1973 with total page 528 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Technical Report by : United States. National Aeronautics and Space Administration
Download or read book NASA Technical Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1974 with total page 886 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Selective Bibliography on High-angle-of-attack Aerodynamics of Aircraft and Aircraft Components at Subsonic Speeds by : Henry W. Woolard
Download or read book A Selective Bibliography on High-angle-of-attack Aerodynamics of Aircraft and Aircraft Components at Subsonic Speeds written by Henry W. Woolard and published by . This book was released on 1974 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Application of the Leading-edge-suction Analogy of Vortex Lift to the Drag Due to Lift of Sharp-edge Delta Wings by : Edward C. Polhamus
Download or read book Application of the Leading-edge-suction Analogy of Vortex Lift to the Drag Due to Lift of Sharp-edge Delta Wings written by Edward C. Polhamus and published by . This book was released on 1968 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Concept of the Vortex Lift of Sharp-edge Delta Wings Based on a Leading-edge-suction Analogy by : Edward Charles Polhamus
Download or read book A Concept of the Vortex Lift of Sharp-edge Delta Wings Based on a Leading-edge-suction Analogy written by Edward Charles Polhamus and published by . This book was released on 1966 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: A concept for the calculation of the vortex lift of sharp-edge delta wings is presented and compared with experimental data. The concept is based on an analogy between the vortex lift and the leading-edge suction associated with the potential flow about the leading-edge. This concept, when combined with potential-flow theory modified to include the nonlinearities associated with the exact boundary condition and the loss of the lift component of the leading-edge suction, provides excellent prediction of the total lift for a wide range of delta wings up to angles of attack 20[degrees] or greater.
Book Synopsis Transonic Pressure Measurements and Comparison of Theory to Experiment for an Arrow-wing Configuration by :
Download or read book Transonic Pressure Measurements and Comparison of Theory to Experiment for an Arrow-wing Configuration written by and published by . This book was released on 1976 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wind tunnel test of an arrow-wing-body configuration consisting of flat and twisted wings as well as a variety of leading- and trailing-edge control surface deflections, was conducted at Mach numbers from 0.4 to 1.1 to provide an experimental pressure data base for comparison with theoretical methods. Theory-to-experiment comparisons of detailed pressure distributions were made using current state-of-the-art attached and separated flow methods. The purpose of these comparisons was to delineate conditions under which these theories are valid for both flat and twisted wings and to explore the use of empirical methods to correct the theoretical methods where theory is deficient. The results are summarized.
Book Synopsis Unsteady Aerodynamic Analysis of Space Shuttle Vehicles. Part 1: Summary Report by :
Download or read book Unsteady Aerodynamic Analysis of Space Shuttle Vehicles. Part 1: Summary Report written by and published by . This book was released on 1973 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuaration by :
Download or read book Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuaration written by and published by . This book was released on 1977 with total page 1152 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP. written by and published by . This book was released on 1970 with total page 1166 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis NASA Contractor Report by : United States. National Aeronautics and Space Administration
Download or read book NASA Contractor Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1976 with total page 518 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Supersonic Cruise Research 1979, Part 1 by :
Download or read book Supersonic Cruise Research 1979, Part 1 written by and published by . This book was released on 1981 with total page 564 pages. Available in PDF, EPUB and Kindle. Book excerpt:
