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Book Longitudinal Aerodynamic Characteristics of Several Thick slab Delta Wings at Mach Numbers of 3 00  4 50  and 6 00 and Angles of Attack to 95 Deg

Download or read book Longitudinal Aerodynamic Characteristics of Several Thick slab Delta Wings at Mach Numbers of 3 00 4 50 and 6 00 and Angles of Attack to 95 Deg written by and published by . This book was released on 1963 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Comparison of Longitudinal Aerodynamic Characteristics of Curved and Straight Leading edge Delta Wings at Mach Numbers 3 and 6

Download or read book Comparison of Longitudinal Aerodynamic Characteristics of Curved and Straight Leading edge Delta Wings at Mach Numbers 3 and 6 written by Dewey E. Wornom and published by . This book was released on 1964 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Transonic Wind tunnel Investigation of the Longitudinal Force and Moment Characteristics of Two Delta Wings and One Clipped tip Delta Wing of 4 Percent Thickness on a Slender Body

Download or read book A Transonic Wind tunnel Investigation of the Longitudinal Force and Moment Characteristics of Two Delta Wings and One Clipped tip Delta Wing of 4 Percent Thickness on a Slender Body written by William E. Palmer and published by . This book was released on 1955 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Longitudinal Aerodynamic Characteristics at Low Subsonic Speeds of a Highly Swept Delta Wing Utilizing Nose Deflection for Control

Download or read book Longitudinal Aerodynamic Characteristics at Low Subsonic Speeds of a Highly Swept Delta Wing Utilizing Nose Deflection for Control written by Bernard Spencer and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book High subsonic speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta wing Configurations for Angles of Attack from 0   to 90

Download or read book High subsonic speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta wing Configurations for Angles of Attack from 0 to 90 written by Bernard Spencer and published by . This book was released on 1959 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Thick Delta Wing Hypersonic Glider Configuration for Angles of Attack Up to 100 Deg

Download or read book Static Longitudinal Aerodynamic Characteristics at Transonic Speeds of a Thick Delta Wing Hypersonic Glider Configuration for Angles of Attack Up to 100 Deg written by and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book High subsonic speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta wing Configurations for Angles of Attack from 0 Deg to 90 Deg

Download or read book High subsonic speed Investigation of the Static Longitudinal Aerodynamic Characteristics of Several Delta wing Configurations for Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2 0

Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2 0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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:

Book Effects of Wing Incidence on the Longitudinal Trim Characteristics of a Cambered 70   Delta wing Configuration at Mach Numbers 3 0 to 5 0

Download or read book Effects of Wing Incidence on the Longitudinal Trim Characteristics of a Cambered 70 Delta wing Configuration at Mach Numbers 3 0 to 5 0 written by Warren F. Ahtye and published by . This book was released on 1960 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Longitudinal Aerodynamic Characteristics at a Mach Number of 1 97 of a Series of Related Winged Reentry Configurations for Angles of Attack from 0 Deg to 90 Deg

Download or read book Longitudinal Aerodynamic Characteristics at a Mach Number of 1 97 of a Series of Related Winged Reentry Configurations for Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1961 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental and Theoretical Study of Longitudinal Aerodynamic Characteristics of Delta and Double delta Wings at Mach Numbers of 1 60  1 90  and 2 16

Download or read book Experimental and Theoretical Study of Longitudinal Aerodynamic Characteristics of Delta and Double delta Wings at Mach Numbers of 1 60 1 90 and 2 16 written by Richard M. Wood and published by . This book was released on 1985 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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.