Prandtl-D

Preliminary Research Aerodynamic Design to Lower Drag, or Prandtl-D is an unmanned experimental glider-aircraft being developed by NASA.[1] The acronym is a reference to early German Aerospace Engineer Ludwig Prandtl.[2]

Prandtl-D
Role Experimental Glider
National origin United States
First flight October 28, 2015
Primary user NASA

The Prandtl-D is a tailless glider that is based on the flight of birds. Birds turn and bank without vertical tails that are required for such maneuvers on traditional aircraft.[3] It is intended to provide for future low drag and experimental aircraft designs, which previously have had issues of controlability. The program reinforced similar wing designs by Ludwig Prandtl which were conceptualized a century before. The Prandtl-D's designs are also based on glider concepts of German brothers Reimar and Walter Horten and incorporate the conclusions of NASA aerodynamics pioneers R.T. Jones and Richard T. Whitcomb.[3]

The Prandtl-D1 and the Prandtl-D3 models were featured in the National Air and Space Museum and the California Science Center, respectively.[4]

Albion Bowers, NASA Armstrong chief scientist and Prandtl-D project manager, brought together the theories and has led the effort with help from student interns.[3] He believes that with the concepts proven under the Prandtl-D "the time may be coming for a new paradigm in aviation."[5]

Development

The first full sized model of these to fly was designated "Prandtl-D No. 3", and flown in a series of tests on October 28, 2015 at the Armstrong Flight Research Center in Edwards, California. The aircraft is centered around the testing of yawing without a vertical stabilizer. The manager of the project, Albion Bowers, said that the aircraft is based on the flight of a bird.[5]

The Prandtl-D No. 3 first flew Oct. 28, 2015, with double the wingspan of the earlier versions,[3] however, through development, the team managed to reduce the final glider's drag by 11%.

Initially, each aircraft was radio operated with a hobby-grade controller and launched with a bungee cord system. Later flight tests switched from a bungee launch method to a towed launch system.[3]

The first two vehicles of the program showed twist of the airfoil in providing an bell shaped lift distribution instead of the elliptical distribution. This feature gave an efficiency boost and reduced strain on the wings.

Later iteration of the vehicle using the bungee launch system

In March 2016, Bowers published a technical paper entitled, “On Wings of the Minimum Induced Drag: Spanload Implications for Aircraft and Birds,” NASA/TP – 2016-219072. Detailing the aerodynamic properties and mathematics associated with the project, Bowers discusses in depth the science behind altering the spanload distribution on aircraft wings and the data gathered from experiments that demonstrated validation of its critical principles.[3][6]

Specifications

The first two subscale Prandtl-D aircraft had a 12.5-foot wingspan and were constructed of a machined foam core wrapped in a skin of carbon fiber.[3] The Prandtl-D No.3 has a wingspan of 25 ft, weight of 28 lbs, top airspeed of 18 kt, and a maximum altitude of 220 ft.[6] The aircraft also has the Arduino flight control system used in the second Prandtl-D subscale model and is constructed of carbon fiber, fiberglass and foam. A key difference in the Prandtl-D full scale model is an addition of a University of Minnesota developed Data Collection System (DAC).[3]

List of Vehicles in the Program
  • Prandtl-D No.3
  • Prandtl-D1
  • Prandtl-D2
  • Prandtl-D3
  • Prandtl-3C

Future platforms

The Prandtl-D lead to start of the Preliminary Research Aerodynamic Design to Land on Mars (Prandtl-M) program designed for Mar's Exploration. It has been tested in upper atmosphere of Earth and is designed to take topographic photos of Mar's surface.

It also has provided a valuable platform for the Weather Hazard Alert and Awareness Technology Radiation Radiosonde Glider (WHAATRR) that will be used for atmospheric weather testing on Earth. [7][6]

“On Wings of the Minimum Induced Drag: Spanload Implications for Aircraft and Birds,” NASA/TP – 2016-219072.

https://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/20160003578.pdf

References
  1. Gibbs, Yvonne (2015-09-21). "Preliminary Research Aerodynamic Design To Lower Drag: An Overview". NASA. Retrieved 2019-07-06.
  2. Bowers, Albion; Murillo, Oscar (March 2016). "On Wings of the Minimum Induced Drag: Spanload Implications for Aircraft and Birds" (PDF). NASA.
  3. "Prandtl-D Aircraft" (PDF). nasa.gov. NASA. 2016. Retrieved 10 November 2019. This article incorporates text from this source, which is in the public domain.
  4. Conner, Monroe (2019-08-06). "Prandtl-D Models Heading to Smithsonian and California Science Center". NASA. Retrieved 2019-11-10.
  5. Conner, Monroe (2016-03-21). "Subscale Glider Validating New Wing Design Method". NASA. Retrieved 2019-11-10.
  6. Gibbs, Yvonne (2017-05-11). "Prandtl-D Aircraft". NASA. Retrieved 2019-07-06.
  7. Conner, Monroe (2017-03-29). "Potential Mars Airplane Resumes Flight". NASA. Retrieved 2019-11-10.
This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.