Wind Tunnel Investigation Of Paraglider Models At Supersonic Speeds PDF Download
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| Author | : Robert T. Taylor |
| Publisher | : |
| Total Pages | : 22 |
| Release | : 1961 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
Download Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds Book in PDF, ePub and Kindle
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of paraglider models at moderate to high supersonic speeds. The models were deployed from a sting in the supersonic stream and steady-state aerodynamics performance data were obtained. Maximum values of the lift-drag ratio were about 1.4 at a Mach number of 2.65 and about 1.2 at a Mach number of 4.65. The angles of attack over which the models could be flown were limited by unsteady behavior of the canopy.
| Author | : Robert T. Taylor (Of the National Aeronautics and Space Administration) |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1961 |
| Genre | : Aerodynamics, Supersonic |
| ISBN | : |
Download Wind-tunnel Investigation of Paraglider Models at Supersonic Speeds Book in PDF, ePub and Kindle
An investigation was made in the Langley Unitary Plan wind tunnel to determine the behavior of paraglider models at moderate to high supersonic speeds. The models were deployed from a sting in the supersonic stream and steady-state aerodynamics performance data were obtained. Maximum values of the lift-drag ratio were about 1.4 at a Mach number of 2.65 and about 1.2 at a Mach number of 4.65. The angles of attack over which the models could be flown were limited by unsteady behavior of the canopy.
| Author | : Nickolai Charczenko |
| Publisher | : |
| Total Pages | : 30 |
| Release | : 1964 |
| Genre | : Drag (Aerodynamics) |
| ISBN | : |
Download Wind-tunnel Investigation of Drag and Stabili- Ty of Parachutes at Supersonic Speeds Book in PDF, ePub and Kindle
| Author | : Francis Melvin Rogallo |
| Publisher | : |
| Total Pages | : 32 |
| Release | : 1960 |
| Genre | : Gliders (Aeronautics) |
| ISBN | : |
Download Preliminary Investigation of a Paraglider Book in PDF, ePub and Kindle
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.
| Author | : L. A. MORGAN |
| Publisher | : |
| Total Pages | : 1 |
| Release | : 1962 |
| Genre | : |
| ISBN | : |
Download Wind Tunnel Investigation of Flexible Parachute Models at Supersonic Speeds Book in PDF, ePub and Kindle
Tests were conducted in the 40-in. Supersonic Tunnel of the von Karman Gas Dynamics Facility to determine the aerodynamic characteristics of a series of flexible parachute models at Mach numbers from 1.5 to 3. Parachutes of various designs employing porous, non-porous, and ribbon materials were tested by deployment from a modified Pershing model. High-speed movies and drag measurements were obtained. (Author).
| Author | : |
| Publisher | : |
| Total Pages | : 482 |
| Release | : 1966 |
| Genre | : |
| ISBN | : |
Download NASA Technical Note Book in PDF, ePub and Kindle
| Author | : Delwin R. Croom |
| Publisher | : |
| Total Pages | : 38 |
| Release | : 1966 |
| Genre | : Paragliding |
| ISBN | : |
Download Low-subsonic Wind-tunnel and Free-flight Drop-test Investigation of a Paraglider Configuration Having Large Tapered Leading Edges and Keel Book in PDF, ePub and Kindle
| Author | : Davis S. Miller |
| Publisher | : |
| Total Pages | : 36 |
| Release | : 1971 |
| Genre | : Airplanes |
| ISBN | : |
Download Wind-tunnel Investigation of Sonic-boom Characteristics of Two Simple Wing Models at Mach Numbers from 2.3 to 4.63 Book in PDF, ePub and Kindle
| Author | : |
| Publisher | : |
| Total Pages | : 77 |
| Release | : 1959 |
| Genre | : Aerodynamic heating |
| ISBN | : |
Download Wind-tunnel Investigation at Subsonic and Supersonic Speeds of Static and Dynamic Stability Derivatives of Airplane Model with Unswept Wing and High Horizontal Tail [with List of References] Book in PDF, ePub and Kindle
| Author | : United States. National Aeronautics and Space Administration |
| Publisher | : |
| Total Pages | : 448 |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
Download Index of N A S A Technical Publications Book in PDF, ePub and Kindle
