Download or read book Tip Aerodynamics from Wind Tunnel Test of Semi span Wing written by and published by . This book was released on 1986 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Exploratory Investigation of the Structure of the Tip Vortex of a Semispan Wing for Several Wing tip Modifications written by James Scheiman and published by . This book was released on 1970 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Method of Determining Aerodynamic influence Coefficients from Wind tunnel Data for Wings at Supersonic Speeds written by Patrick A. Gainer and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation of Aerodynamic Efficiency of Three Planar Elliptical Wings with Curvature of Quarter chord Line written by Raymond E. Mineck and published by . This book was released on 1993 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Low Speed Wind Tunnel Testing written by Alan Pope and published by Wiley-Interscience. This book was released on 1984 with total page 562 pages. Available in PDF, EPUB and Kindle. Book excerpt: Good,No Highlights,No Markup,all pages are intact, Slight Shelfwear,may have the corners slightly dented, may have slight color changes/slightly damaged spine.
Download or read book Experimental Study of an Independently Deflected Wingtip Mounted on a Semispan Wing written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-06 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results of a subsonic wind tunnel test of a semispan wing with an independently deflected tip surface are presented and analyzed. The tip surface was deflected about the quarter chord of the rectangular wing and accounted for 17 percent of the wing semispan. The test was conducted to measure the loads on the tip surface and to investigate the nature of aerodynamic interference effects between the wing and the deflected tip. Results are presented for two swept tip surfaces of similar planform but different airfoil distributions. The report contains plots of tip lift, drag, and pitching moment for various Reynolds numbers and tip deflection angles with respect to the inboard wing. Oil flow visualization photographs for a typical Reynolds number are also included. Important aerodynamic parameters such as lift and pitching moment slopes and tip aerodynamic center location are tabulated. A discussion is presented on the relationship between tip experimental data acquired in a steady flow and the prediction of unsteady tip motion at fixed wing angles of attack. Martin, D. M. and Young, L. A. Ames Research Center...
Download or read book Wind tunnel Testing written by Alan Pope and published by . This book was released on 1954 with total page 536 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Tests of a Swept wing Semispan Model with Circulation Control written by Richard E. Wallace and published by . This book was released on 1953 with total page 214 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large scale Wind tunnel Tests of Descent Performance of an Airplane Model with a Tilt Wing and Differential Propeller Thrust written by Wallace H. Deckert and published by . This book was released on 1964 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted to determine the wing stall, performance, and longitudinal stability and control characteristics of a large model of a V/STOL tilt-wing transport aircraft. The scope of the tests was limited primarily to the low-speed transitional regime.
Download or read book Transonic and Supersonic Wind tunnel Tests of Wing body Combinations Designed for High Efficiency at a Mach Number of 1 41 written by Frederick C. Grant and published by . This book was released on 1960 with total page 86 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental Study of an Independently Deflected Wingtip Mounted on a Semispan Wing written by and published by . This book was released on 1991 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind Tunnel Tests of Fuselages and Windscreens written by Edward Pearson Warner and published by . This book was released on 1925 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt: The tests described herein were made in 1918, in the old four-foot wind tunnel at the Massachusetts Institute of Technology and at the request of the Engineering Division of the U.S. Army Air Service.
Download or read book Large scale Wind tunnel Tests of a Deflected Slipstream STOL Model with Wings of Various Aspect Ratios written by V. Robert Page and published by . This book was released on 1968 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Measurments on Wing Tip Blowing written by Joint Institute for Aeronautics and Acoustics. Joint Institute for Aeronautics and Acoustics and published by . This book was released on 1985 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Wind tunnel Investigation of the Effect of Control Span and Large Wing tip Nacelles on Effectiveness of Spoiler slot Deflector Controls on an Unswept wing Fighter type Airplane written by and published by . This book was released on 1960 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Tabulation of Wind tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1 61 and 2 01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes written by Emma Jean Landrum and published by . This book was released on 1962 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Comparison of Wind tunnel Test Results at M subscript Infinity written by Larry Wayne Mohn and published by . This book was released on 1975 with total page 100 pages. Available in PDF, EPUB and Kindle. Book excerpt:
