Download or read book Low subsonic Aerodynamic Characteristics of a Model of a Fixed wing Space Shuttle Concept at Angles of Attack to 76 written by John P. Decker and published by . This book was released on 1970 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low Subsonic Aerodynamic Characteristics of a Fixed wing Space Shuttle Concept at Angles of Attack to 76 written by John P. Decker and published by . This book was released on 1970 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low subsonic Aerodynamic Characteristics of a Space Shuttle orbiter Concept with a Blended Delta Wing body written by Delma C. Jr Freeman and published by . This book was released on 1971 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Chracteristics of a Fixed wing Manned Space Shuttle Concept at a Mach Number of 6 0 written by David Ray Stone and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Chracteristics of a Fixed wing Manned Space Shuttle Concept at a Mach Number of 6 0 written by David Ray Stone and published by . This book was released on 1970 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Influence of Configuration Details on the Subsonic Characteristics of a Space Shuttle Orbiter Design written by John P. Decker and published by . This book was released on 1974 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Langley s Space Shuttle Technology A Bibliography written by Gloria R. Champine and published by . This book was released on 1981 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of the Low subsonic Stability and Control Characteristics of a 0 34 scale Free flying Model of a Modified Half cone Reentry Vehicle written by James L. Hassell and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of the Low subsonic Aerodynamic Characteristics of a Model of a Modified Lenticular Reentry Configuration written by George M. Ware and published by . This book was released on 1962 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Aerodynamic Characteristics of a Model of a Typical Subsonic Jet transport Airplane at Mach Numbers from 0 40 to 1 20 written by Eugene N. Brooks and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low subsonic Aerodynamic Characteristics of a Shuttle orbiter Configuration with a Variable Dihedral Delta Wing written by and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Configuration Modifications on the Low subsonic Aerodynamic Characteristics of a Space Shuttle orbiter Concept with a Blended Delta Wing body written by Delma C. Jr Freeman and published by . This book was released on 1972 with total page 61 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of the Low subsonic Stability and Control Characteristics of a Free flying Model of a Thick 70 Degree Delta Reentrry Configuration written by John W. Paulson and published by . This book was released on 1961 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Subsonic Static Aerodynamic Characteristics of an Airplane Model Having a Triangular Wing of Aspect Ratio 3 written by Howard F. Savage and published by . This book was released on 1957 with total page 662 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted to determine the effects of vertical-tail location and size on the subsonic aerodynamic characteristics of a model having a triangular wing. The wing had an aspect ratio of 3, an NACA 0003.5-63 section in the streamwise direction, and plain, trailing-edge ailerons. The wing was attached to the fuselage in either a mid or high position and an unswept horizontal tail was located on the fuselage center line. Two vertical tails were tested which had areas of 26.7 or 20.3 percent of the wing area. Each vertical tail was equipped with a rudder and had a geometric aspect ratio of 1.5, a taper ratio of 0.16, and 54 degrees of sweepback of the leading edge. Each vertical tail was tested at two different tail lengths. The wind-tunnel tests were conducted at a Reynolds number of 2.5 milMon at Mach numbers from 0.25 to 0.95.

Download or read book Transonic Investigation of the Static Longitudinal Aerodynamic Characteristics of Low aspect ratio Wing body Configurations at Angles of Attack from 00 to 900 written by Charles D. Trescot 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 Subsonic Aerodynamic Characteristics of a Highly Swept Fixed Wing Configuration with Variation in Wing Dihedral Angle written by William P. Henderson and published by . This book was released on 1971 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: