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 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 Low Subsonic Aerodynamic Characteristics of a 60 Swept Delta wing Space Shuttle Orbiter written by Delma C. Jr Freeman and published by . This book was released on 1973 with total page 55 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 UNITED STATES. NATIONAL AERONAUTICS AND SPACE ADMINISTRATION. and published by . This book was released on 1966 with total page 50 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 Low Subsonic Aerodynamic Characteristics of a Shuttle Orbiter Configuration Designed for Reduced Length written by George M. Ware and published by . This book was released on 1973 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Grumman H 33 Space Shuttle Orbiter Aerodynamic and Handling qualities Study written by and published by . This book was released on 1972 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of a representative delta-wing orbiter, the Grumman H-33, that utilized external-hydrogen tanks has been completed. The study encompassed a detailed wind-tunnel program from subsonic to hypersonic speeds, analyses of the data, and the calculation and assessment of the orbiter handling qualities using the most aft center-of-gravity locations anticipated during entry and approach.

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 60 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low Subsonic Aerodynamic Characteristics of a Shuttle Orbiter Having 35 Trapezoidal Wing and 75 Inboard Glove written by Bernard Jr Spencer and published by . This book was released on 1973 with total page 42 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 1978 with total page 1008 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

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 Low subsonic Longitudinal Aerodynamic Characteristics of a Twin body Space shuttle Booster Configuration written by and published by . This book was released on 1971 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effect of Reynolds Number on the Aerodynamic Stability and Control Characteristics of a 55 Deg Clipped delta wing Orbiter Configuration at Supersonic Mach Numbers written by A. B. Blair (Jr) and published by . This book was released on 1976 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Low subsonic Aerodynamic Characteristics of a Delta wing Recovery Device for Nonlifting Spacecraft written by George M. Ware 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 Investigation of the Low subsonic Flight Characteristics of a Model of a Reentry Vehicle with a Thick Flat 75 Degree Swept Delta Wing and a Half cone Fuselage written by Peter C. Boisseau and published by . This book was released on 1962 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Effects of Reynolds Number and Body Corner Radius on Aerodynamic Characteristics of a Space Shuttle type Vehicle at Subsonic Mach Numbers written by Leland Howard Jorgenson and published by . This book was released on 1972 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static aerodynamic forces and moments were measured to study the effects of Reynolds number and body corner radius on the aerodynamic characteristics of a straight wing space shuttle orbiter at subsonic speeds. A 0.02-scale model was tested at Mach numbers from 0.3 to 0.9 and Reynolds numbers from about 600,000 to 3 million, based on body width. The body alone and the body with its wing and horizontal tail attached were tested at angles of attack from 35 to 75 degrees. The effects of rounding the body corners at the junctures connecting the bottom and sides were investigated for corner radii from 0 to 8.5 percent of the body width. At low subsonic Mach numbers (free stream Mach number approximately equal 0.3) the aerodynamic characteristics are affected significantly by changes in Reynolds number and body corner radius. With increase in Mach number to free stream Mach number = 0.9 the effect of Reynolds number seems to vanish, but a significant effect of body corner radius remains.