Download or read book Effect of Taper Ratio on Lift Drag and Pitching moment Characteristics of Thin Wings of Aspect Ratio 3 with 53 1 Degree Sweepback of Leading Edge at Subsonic and Supersonic Speeds written by Benton E. Wetzel and published by . This book was released on 1955 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Leading edge Sweepback on Lift Drag and Pitching moment Characteristics of Thin Wings of Aspect Ratio 3 and Taper Ratio 0 4 at Subsonic and Supersonic Speeds written by Benton E. Wetzel and published by . This book was released on 1955 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1967 with total page 868 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.
Download or read book The Effects of Circular End Plates on the Lift Drag and Pitching Moment at Subsonic and Supersonic Speeds on a Modified Triangular Wing Having an Aspect Ratio of 2 Taper Ratio of 0 33 and a 45 Degree Swept Leading Edge written by Robert B. Petersen and published by . This book was released on 1954 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Lift Pitching Moment and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio written by Edward J. Hopkins and published by . This book was released on 1951 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0, 35, and 45 degrees. The wing span was decreased to give aspect ratios 6.8, 5.3, 4.2, 3.4, and 2.8. The effects of independent variations of sweep and aspect ratio on the lift, pitching-moment, and span-load characteristics of the wings are compared with the effects estimated by use of the Weissinger method.
Download or read book Lift Drag and Pitching Moment of Low aspect ratio Wings at Subsonic and Supersonic Speeds Plane 45 Degrees Sweptback Wing of Aspect Ratio 3 Taper Ratio 0 4 with 3 percent thick Biconvex Section written by John C. Heitmeyer and published by . This book was released on 1951 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Reports and Memoranda written by and published by . This book was released on 1961 with total page 864 pages. Available in PDF, EPUB and Kindle. Book excerpt: Beginning with no. 650 each hundredth number contains a list of the Reports and memoranda published since the last list.
Download or read book Lift Drag and Pitching Moment of Low aspect ratio Wings at Subsonic and Supersonic Speeds Plane Tapered Wing of Aspect Ratio 3 1 with 3 percent thick Rounded nose Section written by John C. Heitmeyer and published by . This book was released on 1952 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book The Lift Drag and Pitching Moment of Three Unswept Wings of Aspect Ratio 3 5 and Taper Ratio 0 5 with Different Wing Sections at Transonic and Supersonic Speeds written by J. B. Scott-Wilson and published by . This book was released on 1955 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Engineering Review written by and published by . This book was released on 1957 with total page 1846 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Supersonic Lift and Pitching Moment of Thin Sweptback Tapered Wings Produced by Constant Vertical Acceleration written by and published by . This book was released on 1951 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt: Theoretical approximations to the nondimensional lift and pitching moment produced by constant vertical acceleration, the CL(alpha) and CM(alpha) derivatives, respectively, are derived for a series of thin sweptback tapered wings with streamwise tips. The analysis is essentially the application of a recently published solution of the linearized time-dependent wave equation for wings in accelerated motion. The results are independent of camber and thickness and are applicable for a range of supersonic speed for which the wing is wholly contained between the Mach cones springing from the wing apex and from the trailing edge of the root section (subsonic leading edge and supersonic trailing edge). Design curves are presented which permit rapid estimation of the derivatives CL(alpha) and CM(alpha) for given values of aspect ratio, taper ratio, Mach number, and leading-edge sweep.
Download or read book Lift Drag and Pitching Moment of Low aspect ratio Wings at Subsonic and Supersonic Speeds written by Ronald C. Hightower and published by . This book was released on 1953 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerospace Engineering written by and published by . This book was released on 1958-05 with total page 1236 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Lift Drag and Pitching Moment of Low aspect ratio Wings at Subsonic and Supersonic Speeds Plane Tapered Wing of Aspect Ratio 3 1 with 3 Percent thick Biconvex Section written by David E. Reese and published by . This book was released on 1951 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Lift Drag and Pitching Moment of Low aspect ratio Wings at Subsonic and Supersonic Speeds Plane Triangular Wing of Aspect Ratio 3 with NACA 0003 63 Section written by John C. Heitmeyer and published by . This book was released on 1951 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: A wing-body combination having a plane triangular wing of aspect ratio 3 and NACA 0003-63 sections in streamwise planes has been investigated at both subsonic and supersonic Mach numbers. The lift, drag, and pitching moment of the model are presented for Mach numbers from 0.60 to 0.92 and from 1.20 to 1.70 at a Reynolds number of 4.80 million. The variations of the characteristics with Reynolds number are also shown for several Mach numbers.
Download or read book Damping in pitch Characteristics at High Subsonic and Transonic Speeds of Four 35 Sweptback Wings written by William B. Kemp and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Lift Drag and Pitching Moment of Low aspect ratio Wings at Subsonic and Supersonic Speeds an Investigation at Large Reynolds Numbers of the Low speed Characteristics of Several Wing body Combinations written by Donald W. Smith and published by . This book was released on 1952 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
