Download or read book Investigation of the Effects of Leading edge Chord extensions on the Aerodynamic and Control Characteristics of Two Sweptback Wings at Mach Numbers of 1 41 1 62 and 1 96 written by Ellery B. Jr May and published by . This book was released on 1951 with total page 25 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index to NASA Technical Publications written by United States. National Aeronautics and Space Administration and published by . This book was released on 1960-07 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Effects of Leading edge Chord extensions and Fences in Combination with Leading edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0 40 to 0 93 of a 45 Degree Sweptback Wing of Aspect Ratio 4 written by Kenneth P. Spreemann and published by . This book was released on 1953 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Leading edge Chord extensions on the Aerodynamic Characteristics of a 45 Degrees Sweptback Wing fuselage Combination at Mach Numbers of 0 40 to 1 03 written by F.E. Jr West and published by . This book was released on 1953 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Leading edge Chord extensions on the Aerodynamic Characteristics of a 45 Sweptback Wing fuselage Combination at Mach Numbers of 0 40 to 1 03 written by and published by . This book was released on 1953 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on with total page 1284 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Flight Investigation of the Effects of a Partial span Leading edge Chord Extension on the Aerodynamic Characteristics of a 35 Degree Swept wing Fighter Airplane written by Frederick H. Matteson and published by . This book was released on 1954 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation of the Aerodynamic Characteristics at High Supersonic Mach Numbers of a Family of Delta Wings Having Double wedge Sections with the Maximum Thickness at 0 18 Chord written by Mitchel H. Bertram and published by . This book was released on 1954 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt: A program to investigate the aerodynamic characteristics of a family of delta wings with a blunt double-wedge section has been conducted at the Langley 11-inch hypersonic tunnel. These wings had a maximum thickness of 8 percent of the chord located at the 18-percent-chord point. For the wings tested at a Mach number of 6.9, the semiapex angle was varied from 5 to 30 degrees and the wings were tested over a range of angle of attack from 0 to 28 degrees and Reynolds numbers in the range of 800,000 to 3,600,000 based on root chord. In addition, pertinent results from tests at Mach number as low as 1.62 have been utilized. The shock-expansion theory and the Newtonian impact theory have been used to analyze the effects of changes made in the various parameters investigated.
Download or read book Effects of Wing Planform on the Aerodynamic Characteristics of a Wing body tail Model at Mach Numbers 1 57 2 16 and 2 87 written by Royce L. McKinney and published by . This book was released on 1965 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Leading edge Chord extensions on Subsonic and Transonic Aerodynamic Characteristics of Three Models Having 45 Degree Sweptback Wings of Aspect Ratio 4 written by Kenneth W. Goodson and published by . This book was released on 1953 with total page 31 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects at Mach Numbers of 1 61 and 2 01 of Camber and Twist on the Aerodynamic Characteristics of Three Swept Wings Having the Same Planform written by Emma Jean Landrum and published by . This book was released on 1961 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Leading edge Chord extensions on Subsonic and Transonic Aerodynamic Characteristics of Three Models Having 45 Degrees Sweptback Wings of Aspect Ratio 4 written by Kenneth W. Goodson and published by . This book was released on 1953 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Systematic Study of the Effects of Leading edge Chord extensions on the Low speed Longitudinal Stability Characteristics of Three 45 Degree Sweptback Wings written by H. Neale Kelly and published by . This book was released on 1955 with total page 113 pages. Available in PDF, EPUB and Kindle. Book excerpt: A low-speed leading-edge chord-extension has been conducted in the Langley 19-foot pressure tunnel. In the course of the investigation, chord-extensions of various designs were tested on three 45 degree sweptback wings of aspect ratio 5 and taper ratio 0.28 incorporating different airfoil sections. The tests were made at a Reynolds number of 4,600,000 and a corresponding Mach number of 0.11.
Download or read book Effects of Wing crank Leading edge Chord Extensions and Horizontal tail Height on the Longitudinal Stability of Swept wing Models at Mach Numbers from 0 6 to 1 4 written by Roy M. Wakefield and published by . This book was released on 1959 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effect of Skewed Wing tip Controls on a Highly Swept Arrow Wing at Mach Number 2 03 written by Emma Jean Landrum and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book FLIGHT INVESTIGATION OF THE EFFECTS OF A PARTIAL SPAN LEADING EDGE CHORD EXTENSION ON THE AERODYNAMIC CHARACTERISTICS OF A 35 Deg SWEPT WING FIGHTER AIRPLANE written by and published by . This book was released on 1954 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Systematic Study of the Effects of Leading edge Chord extension on the Low speed Longitudinal Stability Characteristics of Three 45 Degrees Sweptback Wings written by H. Neale Kelly and published by . This book was released on 1955 with total page 113 pages. Available in PDF, EPUB and Kindle. Book excerpt:
