Download or read book Investigation at Mach Numbers of 0 20 to 3 50 of a Blended Diamond Wing and Body Combination of Sonic Design But with Low Wave drag Increase with Increasing Mach Number written by George H. Holdaway and published by . This book was released on 1959 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation at Mach Numbers of 0 20 to 3 50 of Blended Wing body Combinations of Sonic Design with Diamond Delta and Arrow Plan Forms written by George H. Holdaway and published by . This book was released on 1960 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation at Mach Numbers of 0 20 to 3 50 of a Blended Diamond Wing and Body Combination of Sonic Design But with Low Wave drag Increase with Increasing Mach Number written by George H. Holdaway and published by . This book was released on 1959 with total page 58 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 at Mach Numbers of 0 20 to 3 50 of Blended Wing body Combinations of Sonic Design with Diamond Delta and Arrow Plan Forms with List of References written by and published by . This book was released on 1960 with total page 77 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation at Mach Numbers of 0 60 to 3 50 of Blended Wing body Combinations with Cambered and Twisted Wings with Diamond Delta and Arrow Plan Forms written by George H. Holdaway and published by . This book was released on 1961 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Download or read book Evaluation of Blended Wing body Combinations with Curved Plan Forms at Mach Numbers Up to 3 50 written by George H. Holdaway and published by . This book was released on 1960 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback wing body Combination Designed for High Performance written by Donald L. Loving and published by . This book was released on 1961 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation at Mach Numbers of 0 60 to 3 50 of Blended Wing body Combinations with Cambered and Twisted Wings with Diamond Delta and Arrow Plan Forms with List of References written by and published by . This book was released on 1960 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free flight Measurements of the Zero lift Drag of Several Wings at Mach Numbers from 1 4 to 3 8 written by H. Herbert Jackson and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Investigation at Mach Numbers of 0 06 to 3 50 of Blended Wing Body Combinations with Cambered and Twisted Wing with Diamond Delta and Arrow Plan Forms written by George H. Holdaway and published by . This book was released on 1960 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Investigation at Mach Numbers from 0 20 to 4 63 of the Aerodynamic Performance Static Stability and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight written by and published by . This book was released on 1961 with total page 88 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Effectiveness of an All movable Horizontal Tail on an Unswept wing and Body Combination for Mach Numbers from 0 60 to 1 40 written by Louis S. Stivers and published by . This book was released on 1959 with total page 28 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 Investigation of the Drag of Blunt nosed Bodies of Revolution in Free Flight at Mach Numbers from 0 6 to 2 3 written by Harvey A. Wallskog and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Measurements of the Mach Number and Pressure on the Afterbody of a Blunt nosed Model in Free Flight at Mach Numbers from 6 5 to 14 written by Simon C. Sommer and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
