Comparison Of The 10x10 And The 8x6 Supersonic Wind Tunnels At The Nasa Glenn Research Center For Low Speed Subsonic Operation
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Bringing the Future Within Reach
| Author | : Robert S. Arrighi |
| Publisher | : Government Printing Office |
| Total Pages | : 428 |
| Release | : 2016 |
| Genre | : Technology & Engineering |
| ISBN | : 9780160932106 |
The book documents Glenn's many research specialties over those 75 years. Among them are early jet engines and rockets; flight safety and fuel efficiency tested in premier icing and wind tunnels; liquid hydrogen fuel which, despite skeptics like aerospace engineer Wernher von Braun, helped the U.S. win the race to the moon; and electric propulsion, considered key to future space flight. Space enthusiasts, aviation personnel, aerospace engineers, and inventors may be interested in this comprehensive and milestone volume. Other related products: NASA at 50: Interviews With NASA\'s Senior Leadership can be found here: https: //bookstore.gpo.gov/products/sku/033-000-01360-4 Other products published by National Aeronautical and Space Administration (NASA) can be found here: https: //bookstore.gpo.gov/agency/550
Scientific and Technical Aerospace Reports
| Author | : |
| Publisher | : |
| Total Pages | : 456 |
| Release | : 1995 |
| Genre | : Aeronautics |
| ISBN | : |
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.
Experimental Investigation of a Large-scale, Two-dimensional, Mixed-compression Inlet System
| Author | : Norman D. Wong |
| Publisher | : |
| Total Pages | : 68 |
| Release | : 1971 |
| Genre | : Jet engines |
| ISBN | : |
A large-scale, variable-geometry inlet model with a design Mach number of 3.0 was tested at Mach numbers from 1.55 to 3.2. Variable features of the inlet for off-design operation are an adjustable-height ramp system and a translating cowl. This report presents experimental results for a diffuser and boundary-layer bleed configuration which was optimized at the design Mach number. Overall performance was high with throat-mounted vortex generators, which were effective in reducing flow distortion in the subsonic diffuser at the higher Mach numbers.
Science in Flux
| Author | : Mark D. Bowles |
| Publisher | : Government Printing Office |
| Total Pages | : 376 |
| Release | : 2006 |
| Genre | : Nuclear energy |
| ISBN | : 9780160877377 |
Revolutionary Atmosphere
| Author | : Robert S. Arrighi |
| Publisher | : |
| Total Pages | : 412 |
| Release | : 2011-03-01 |
| Genre | : Science |
| ISBN | : 9781780393728 |
NASA SP 2010-4319. NASA History Series. This scholarly look at the Altitude Wind Tunnel covers the transformations the wind tunnel made in its long history from a wind tunnel doing full-scale testing for wartime applications, to a vacuum chamber supporting the Vision for Space Exploration, and even a brief period as home to Mercury astronaut training. The book also addresses the attempts to resurrect the facility and its eventual decommissioning and demolition.
Acquisition and utilization of wind tunnels by the National Aeronautics and Space Administration
| Author | : United States. General Accounting Office |
| Publisher | : |
| Total Pages | : 230 |
| Release | : 1976 |
| Genre | : Aerodynamics |
| ISBN | : |
Taming Liquid Hydrogen: The Centaur Upper Stage Rocket 1958-2002
| Author | : |
| Publisher | : Government Printing Office |
| Total Pages | : 310 |
| Release | : 2004 |
| Genre | : Centaur rocket |
| ISBN | : 9780160877391 |
