NASA Technical Reports Server (NTRS) : Exploratory pdf

NASA Technical Reports Server (NTRS) : Exploratory

More Book Details

Description of the Book:

Longitudinal and lateral-directional characteristics of a simple biwing configuration were determined over an angle-of-attack range from -3 deg to 50 deg. The body was comprised of a cylindrical section with an ogival forebody having an overall fineness ratio of 6.67. The delta wings had a 38.3 deg sweep angle and were geometrically similar in planform. The upper wing was located slightly forward relative to the lower wing. The model was tested in upright and inverted orientations including component buildups. This investigation was conducted in the 22-inch aerodynamics leg of the Langley Hypersonic Helium Tunnel Facility

• Creator/s: NASA Technical Reports Server (NTRS
• Date: 2/1/1984
• Year: 1984
• Book Topics/Themes: NASA Technical Reports Server (NTRS), AERODYNAMIC CHARACTERISTICS, AERODYNAMIC CONFIGURATIONS, DELTA WINGS, MACH NUMBER, ANGLE OF ATTACK, FLOW VISUALIZATION, HYPERSONIC SPEED, WIND TUNNEL TESTS, Bernot, P. T

An excerpt captured from the PDF book