Download or read book STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF SEVERAL WING AND BLUNT BODY SHAPES APPLICABLE FOR USE AS REENTRY CONFIGURATIONS AT A MACH NUMBER OF 6 8 AND ANGLES OF ATTACK UP TO 90 DEG written by and published by . This book was released on 1959 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research on Blunt faced Entry Configurations at Angles of Attack Between 60 and 90 written by William H. Phillips and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by and published by . This book was released on 1963 with total page 500 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Longitudinal Aerodynamic Characteristics of Several Wing and Blunt body Shapes Applicable for Use as Reentry Configurations at a Mach Number of 6 8 and Angles of Attack Up to 90 written by Jim A. Penland and published by . This book was released on 1959 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aerodynamic Characteristics of a Group of Winged Reentry Vehicles at Mach Number 6 01 at Angles of Attack from 60 Deg to 120 Deg and Minus 10 Deg to 30 Deg Roll at 90 Deg Angle of Attack written by and published by . This book was released on 1961 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Pressure Distributions on Blunt Delta Wings at a Mach Number of 2 91 and Angles of Attack Up to 90 Deg written by and published by . This book was released on 1962 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Research on Blunt faced Entry Configurations at Angles of Attack Between 60 Deg and 90 Deg written by and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Approximate Analysis of Atmospheric Entry Corridors and Angles written by Roger W. Luidens and published by . This book was released on 1961 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Static Stability and Control Characteristics of a Proposed Winged Reentry Vehicle at Mach Numbers of 1 50 2 96 and 4 63 written by and published by . This book was released on 1962 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Theoretical and Experimental Longitudinal and Lateral Static Stability and Control Characteristics of a Series of Axisymmetric High Drag Reentry Vehicles at a Mach Number of 6 7 written by and published by . This book was released on 1963 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Wind tunnel Investigation of the Aerodynamic Characteristics of a Generalized Series of Winged Reentry Configurations at Angles of Attack to 180 Deg at Mach Numbers of 2 38 2 99 and 4 00 written by and published by . This book was released on 1961 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effects of Rounding Corners and Leading Edges on the Windward surface Pressures of a Delta Wing Swept 650 at a Mach Number of 5 96 at Angles of Attack from 650 to 1150 and Angles of Roll from O0 to 250 at 900 Angle of Attack written by Theodore J. Goldberg and published by . This book was released on 1963 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Exploratory Investigation at a Mach Number of 6 9 Into the Use of Aerodynamic Controls for Modulating the Lift drag Ratio of an Apollo Type Configuration written by and published by . This book was released on 1963 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Summary of Aerodynamic Characteristics of Low lift drag ratio Reentry Vehicles from Subsonic to Hypersonic Speeds written by and published by . This book was released on 1961 with total page 306 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Fixed base Simulation Study of a Pilot s Ability to Control a Winged satellite Vehicle During High drag Variable lift Entries written by John Marshall Eggleston and published by . This book was released on 1960 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Method for Predicting the Normal force Characteristics of Delta Wings at Angles of Attack from 0 Deg to 90 Deg written by and published by . This book was released on 1963 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Fixed base Simulation Study of a Pilot s Ability to Control a Winged satellite Vehicle During High drag Variable lift Entries written by John M. Eggleston and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
