Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Low Subsonic Wind Tunnel And Free Flight Drop Test Investigation Of A Paraglider Configuration Having Large Tapered Leading Edges And Keel PDF full book. Access full book title Low Subsonic Wind Tunnel And Free Flight Drop Test Investigation Of A Paraglider Configuration Having Large Tapered Leading Edges And Keel.
| Author | : Delwin R. Croom |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1966 |
| Genre | : Paragliding |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 440 |
| Release | : 1968 |
| Genre | : |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1492 |
| Release | : 1966 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 2300 |
| Release | : 1967 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : James H. Siviter |
| Publisher | : |
| Total Pages | : 52 |
| Release | : 1968 |
| Genre | : Detectors |
| ISBN | : |
| Author | : United States. Superintendent of Documents |
| Publisher | : |
| Total Pages | : 766 |
| Release | : 1967 |
| Genre | : Government publications |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 2084 |
| Release | : 1967 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division |
| Publisher | : |
| Total Pages | : 2088 |
| Release | : 1966 |
| Genre | : Aeronautics |
| ISBN | : |
| Author | : |
| Publisher | : |
| Total Pages | : 1466 |
| Release | : 1966 |
| Genre | : Government publications |
| ISBN | : |
| Author | : Francis Melvin Rogallo |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1960 |
| Genre | : Gliders (Aeronautics) |
| ISBN | : |
A preliminary investigation of the aerodynamic and control characteristics of a flexible glider similar to a parachute in construction has been made at the Langley Research Center to evaluate its capabilities as a reentry glider. Preliminary weight estimates of the proposed vehicle indicate that such a structure can be made with extreamly low wing loading. Maximum temperatures during the reentry maneuver might be held as low as about 1,500 degrees F.
