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Author : Alexander Lippisch
Publisher : Iowa State Press
ISBN 13 :
Total Pages : 144 pages
Book Rating : 4.63/5 ( download)
Download or read book The Delta Wing written by Alexander Lippisch and published by Iowa State Press. This book was released on 1981 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt: Den tyske flykonstruktør beskriver her udviklingen og forsøgene med Tailless- og Delta Wing- flytyper.
Author :
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.2O/5 ( download)
Download or read book Swept and Delta Wing Sense written by and published by . This book was released on 1955 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : David E. Fetterman
Publisher :
ISBN 13 :
Total Pages : 72 pages
Book Rating : 4.89/5 ( download)
Download or read book An Analysis of the Delta-wing Hypersonic Stability and Control Behavior at Angles of Attack Between 30° and 90° written by David E. Fetterman and published by . This book was released on 1963 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Raymond E. Gordnier
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.38/5 ( download)
Download or read book Unsteady Navier-Stokes Solutions for a Low Aspect Ratio Delta Wing written by Raymond E. Gordnier and published by . This book was released on 1990 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: A numerical investigation of the flow field about a 76-degree leading edge sweep delta wing at 20.5 degree angle of attack is presented. The computational results are obtained using a Beam-Warming algorithm with a Newton-like subiteration procedure. For M = 0.2 and Re = 900,000 an unsteady flow field is obtained which is shown to be physical in nature. The unsteady behaviour is a result of the existence of small-scale vortical structures that are associated with a Kelvin-Helmholtz type instability of the shear layer emanating form the leading edge of the delta wing. The computed results show qualitative agreement with other experimental and numerical findings.
Author : John M. Riebe
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.73/5 ( download)
Download or read book Low-speed Static Stability Characteristics of a Cambered-delta-wing Model written by John M. Riebe and published by . This book was released on 1956 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley 300 MPH 7- by 10-foot tunnel to determine the static stability characteristics of a cambered-delta-wing model. The cambered delta wing was derived from a segment of a cone selected so that the projected plan form with a wing dihedral angle of zero degrees was the same as a 60 degree delta wing. The projected plan form had an aspect ratio of 2.31.
Author : Robert W. Dunning
Publisher :
ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.99/5 ( download)
Download or read book Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number of 4.04 written by Robert W. Dunning and published by . This book was released on 1953 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Raymond E. Gordnier
Publisher :
ISBN 13 :
Total Pages : 50 pages
Book Rating : 4.71/5 ( download)
Download or read book Computation of a Delta-wing Roll-and-hold Maneuver written by Raymond E. Gordnier and published by . This book was released on 1993 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents computations of the flowfield around an 80 degree sweep delta wing undergoing a constant roll-rate maneuver from 0 to 45 degrees. The governing equations for the problem are the unsteady, three- dimensional Navier-Stokes equations. The equations are solved using the implicit, approximately-factored algorithm of Beam-Warming. Fixed roll angle results are also presented and compared with experimental measurements to demonstrate the ability of the numerical technique to accurately capture the flowfield around a rolled delta wing. The dynamic behaviors of the vortex position and strength, as well as their corresponding effect on surface pressure, lift and roll moment, are described. A simple, quasi-static explanation of these vortex behaviors based on effective angle-of-attack and sideslip angle is proposed ... Delta wing roll, Vortex dynamics, Vortical flow, Unsteady maneuver.
Author : John A. Moore
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.77/5 ( download)
Download or read book Experimental Determination of Damping in Pitch of Swept and Delta Wings at Supersonic Mach Numbers written by John A. Moore and published by . This book was released on 1957 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: The damping-in-pitch derivative was determined experimentally at Mach numbers of 2.96 and 3.92 for two delta wings having aspect ratios of 2 and 3 and for one sweptback tapered wing having an aspect ratio of 3 by using a free-oscillation technique. The tests were made at Reynolds numbers based on mean aerodynamic chord from 4,000,000 to 12,000,000 for an angle-of-attack range of zero to 10 degrees. The reduced-frequency parameter ranged from 0.006 to 0.022.
Author : Thomas G. Gainer
Publisher :
ISBN 13 :
Total Pages : 82 pages
Book Rating : 4.20/5 ( download)
Download or read book A Discrete-Vortex Method for Studying the Wing Rock of Delta Wings written by Thomas G. Gainer and published by . This book was released on 2002 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. Wayne Keyes
Publisher :
ISBN 13 :
Total Pages : 52 pages
Book Rating : 4.53/5 ( download)
Download or read book Pressures and Heat Transfer on a 75 ̊swept Delta Wing with Trailing-edge Flap at Mach 6 and Angles of Attack to 90 written by J. Wayne Keyes and published by . This book was released on 1969 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure and heat transfer on swept delta wing with trailing-edge flap.
