The Langley 14- by 22-foot Subsonic Tunnel PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download The Langley 14- by 22-foot Subsonic Tunnel PDF full book. Access full book title The Langley 14- by 22-foot Subsonic Tunnel by Garl L. Gentry. Download full books in PDF and EPUB format.

The Langley 14- by 22-foot Subsonic Tunnel

The Langley 14- by 22-foot Subsonic Tunnel PDF Author: Garl L. Gentry
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 76

Book Description


The Langley 14- by 22-foot Subsonic Tunnel

The Langley 14- by 22-foot Subsonic Tunnel PDF Author: Garl L. Gentry
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 76

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 68

Book Description


Langley Aerospace Test Highlights, 1988

Langley Aerospace Test Highlights, 1988 PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 172

Book Description
Some of the significant tests which were performed during calendar year 1988 in Langley test facilities, a number of which are unique in the world are highlighted.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 160

Book Description


Low Reynolds Number Aerodynamics

Low Reynolds Number Aerodynamics PDF Author: Thomas J. Mueller
Publisher: Springer Science & Business Media
ISBN: 3642840108
Category : Science
Languages : en
Pages : 456

Book Description
Current interest in a variety of low Reynolds number applications has focused attention on the design and evaluation of efficient airfoil sections at chord Reynolds numbers from about 100,000 to about 1,000,000. These applications include remotely piloted vehicles (RPVs) at high altitudes, sailplanes, ultra-light man-carrying/man powered aircraft, mini-RPVs at low altitudes and wind turbines/propellers. The purpose of this conference was to bring together those researchers who have been active in areas closely related to this subject. All of the papers presented are research type papers. Main topics are: Airfoil Design and Analysis, Computational Studies, Stability and Transition, Laminar Separation Bubble, Steady and Unsteady Wind Tunnel Experiments and Flight Experiments.

Monthly Catalogue, United States Public Documents

Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1100

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1100

Book Description


Effect of Planform Taper on Hover Performance of an Advanced AH-64 Model Rotor

Effect of Planform Taper on Hover Performance of an Advanced AH-64 Model Rotor PDF Author: Henry L. Kelley
Publisher:
ISBN:
Category : Rotors (Helicopters)
Languages : en
Pages : 16

Book Description