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Author : James J. Gallagher
Publisher :
ISBN 13 :
Total Pages : 41 pages
Book Rating : 4.:/5 (11 download)
Download or read book Preliminary Tests to Determine the Maximum Lift of Wings at Supersonic Speeds written by James J. Gallagher and published by . This book was released on 1947 with total page 41 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Macon C. Ellis
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)
Download or read book Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings written by Macon C. Ellis and published by . This book was released on 1949 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results from a supersonic wind-tunnel investigation of a series of thin triangular and sweptback wings are presented. The triangular wing series consisted of eight triangular wings of vertex angles such that a range of leading-edge postions both inside and outside the Mach cone at the test Mach numbers of 1.43 and 1.71 was obtained. The three swept wings had angles of sweep at 45, 55, and 63 degrees and were tested at a Mach number of 1.43.
Author : James J. Gallagher
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (248 download)
Download or read book An Investigation of the Maximum Lift of Wings at Supersonic Speeds written by James J. Gallagher and published by . This book was released on 1955 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : John P. Mayer
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.3/5 (91 download)
Download or read book Estimation of Lift and Drag of Airfoils at Near Sonic Speeds and in the Presence of Detached Shock Waves written by John P. Mayer and published by . This book was released on 1949 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Macon C Ellis (Jr)
Publisher :
ISBN 13 :
Total Pages : 37 pages
Book Rating : 4.:/5 (249 download)
Download or read book Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings written by Macon C Ellis (Jr) and published by . This book was released on 1949 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Max A. Heaslet
Publisher :
ISBN 13 :
Total Pages : 726 pages
Book Rating : 4.F/5 ( download)
Download or read book The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms written by Max A. Heaslet and published by . This book was released on 1948 with total page 726 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 242 pages
Book Rating : 4.F/5 ( download)
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1955 with total page 242 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Richard T. Whitcomb
Publisher :
ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)
Download or read book A Supersonic Area Rule and an Application to the Design of a Wing-body Combination with High Lift-drag Ratios written by Richard T. Whitcomb and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: Summary: As an extension of the transonic area rule, a concept for interrelating the wave drags of wing-body combinations at moderate supersonic speeds with axial developments of cross-sectional area has been derived. The wave drag of a combination at a given supersonic speed is related to a number of developments of cross-sectional areas as intersected by Mach planes. On the basis of this concept and other design procedures, a structurally feasible, swept-wing--indented-body combination has been designed to have relatively high maximum lift-drag ratios over a range of transonic and moderate supersonic Mach numbers. The wing of the combination has been designed to have reduced drag associated with lift and, when used with an indented body, to have low zero-lift wave drag. Experimental results have been obtained for this configuration at Mach numbers from 0.80 to 2.01. Maximum lift-drag ratios of approximately 14 and 9 were measured at Mach numbers of 1.15 and 1.41, respectively.
Author : Macon C. Jr Ellis
Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.:/5 (11 download)
Download or read book Preliminary Tests at Supersonic Speeds of Triangular and Swept-back Wings written by Macon C. Jr Ellis and published by . This book was released on 1947 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jesse L. Mitchell
Publisher :
ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Static and Dynamic Longitudinal Stability Characteristics of Some Supersonic Aircraft Configurations written by Jesse L. Mitchell and published by . This book was released on 1952 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Charles H. McLellan
Publisher :
ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.3/5 (91 download)
Download or read book Factors Affecting the Maximum Lift-drag Ratio at High Supersonic Speeds written by Charles H. McLellan and published by . This book was released on 1956 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the factors affecting the maximum lift-drag ratio has been conducted in an effort to determine how to obtain high aerodynamic values at high supersonic Mach numbers.
Author :
Publisher :
ISBN 13 :
Total Pages : 750 pages
Book Rating : 4.X/5 (4 download)
Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Sidney R. Alexander
Publisher :
ISBN 13 :
Total Pages : 8 pages
Book Rating : 4.:/5 (716 download)
Download or read book Flight Tests to Determine the Effect of Taper on the Zero-lift Drag of Wings at Low Supersonic Speeds written by Sidney R. Alexander and published by . This book was released on 1947 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted on wings having taper ratios from 0 to 1 mounted on rocket propelled test bodies to determine the effect of taper on the zero lift drag of wings at low supersonic speeds. Detailed data on models and test conditions are provided. comparison is made between results of theoretical drag calculations of tapered wings and applicable experimental values derived. Maximum thickness, leading edge, and trailing edge sweep are used in determining drag coefficient. At a constant leading edge sweep of 45 degree, no orderly variation of drag coefficient with taper ratio occurs.
Author : Clarence L. Gillis
Publisher :
ISBN 13 :
Total Pages : 44 pages
Book Rating : 4.3/5 (91 download)
Download or read book Flight Tests at Transonic and Supersonic Speeds of an Airplane-like Configuration with a Thin Straight Sharp-edge Wings and Tail Surfaces written by Clarence L. Gillis and published by . This book was released on 1949 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : United States. National Advisory Committee for Aeronautics
Publisher :
ISBN 13 :
Total Pages : 10 pages
Book Rating : 4.3/5 (126 download)
Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1952 with total page 10 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Murray Pittel
Publisher :
ISBN 13 :
Total Pages : 23 pages
Book Rating : 4.:/5 (719 download)
Download or read book Flight Tests at Supersonic Speeds to Determine the Effect of Taper on the Zero-lift Drag of Sweptback Low-aspect-ratio Wings written by Murray Pittel and published by . This book was released on 1950 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: Rocket-powered models have been flown to provide an experimental comparison with linearized theoretical calculations for zero-lift drag of sweptback tapered wings having thin, symmetrical, double-wedge airfoil sections. The range of the experimental data is from Mach number 1.0 to 1.8, and theoretical comparisons are made for the test range above M = 1.2.
Author : Charles T. D'Aiutolo
Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)
Download or read book Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback written by Charles T. D'Aiutolo and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
