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On Span And Space by Bjorn Sandaker

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1Off-design Correlation For Losses Due To Part-Span Dampers On Transonic Rotors... NASA Technical Paper 1693... Scientific And Technical Information Branch, Natl. Aeronautics And Space Administration... Jul. 1980

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NAS 1.60:1693 Digitized from IA1177308-05-0105 .

“Off-design Correlation For Losses Due To Part-Span Dampers On Transonic Rotors... NASA Technical Paper 1693... Scientific And Technical Information Branch, Natl. Aeronautics And Space Administration... Jul. 1980” Metadata:

  • Title: ➤  Off-design Correlation For Losses Due To Part-Span Dampers On Transonic Rotors... NASA Technical Paper 1693... Scientific And Technical Information Branch, Natl. Aeronautics And Space Administration... Jul. 1980
  • Author: ➤  
  • Language: English

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The book is available for download in "texts" format, the size of the file-s is: 39.09 Mbs, the file-s for this book were downloaded 68 times, the file-s went public at Wed Jul 13 2022.

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2NASA Technical Reports Server (NTRS) 19770013203: Supersonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC Unitary Plan Wind Tunnel (LA49)

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A wind tunnel test is reported on an early version of the space shuttle orbiter (designated 089B-139) 0.0165 scale model to systematically determine both longitudinal and lateral control effectiveness associated with various combinations of inboard, outboard, and full span wing trailing edge controls. The test Mach umbers were 2.5 and 4.63 over an angle of attack range from -4 deg to 42 deg at 0 deg sideslip.

“NASA Technical Reports Server (NTRS) 19770013203: Supersonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC Unitary Plan Wind Tunnel (LA49)” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19770013203: Supersonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC Unitary Plan Wind Tunnel (LA49)
  • Author: ➤  
  • Language: English

“NASA Technical Reports Server (NTRS) 19770013203: Supersonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC Unitary Plan Wind Tunnel (LA49)” Subjects and Themes:

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The book is available for download in "texts" format, the size of the file-s is: 83.88 Mbs, the file-s for this book were downloaded 67 times, the file-s went public at Tue Jul 26 2016.

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3On Span And Space : Exploring Structures In Architecture

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A wind tunnel test is reported on an early version of the space shuttle orbiter (designated 089B-139) 0.0165 scale model to systematically determine both longitudinal and lateral control effectiveness associated with various combinations of inboard, outboard, and full span wing trailing edge controls. The test Mach umbers were 2.5 and 4.63 over an angle of attack range from -4 deg to 42 deg at 0 deg sideslip.

“On Span And Space : Exploring Structures In Architecture” Metadata:

  • Title: ➤  On Span And Space : Exploring Structures In Architecture
  • Author:
  • Language: English

“On Span And Space : Exploring Structures In Architecture” Subjects and Themes:

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The book is available for download in "texts" format, the size of the file-s is: 746.91 Mbs, the file-s for this book were downloaded 47 times, the file-s went public at Sun Jul 09 2023.

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4NASA Technical Reports Server (NTRS) 19770013202: Transonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC 8-foot Transonic Wind Tunnel (LA48)

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A transonic pressure tunnel test is reported on an early version of the space shuttle orbiter (designated 089B-139) 0.0165 scale model to systematically determine both longitudinal and lateral control effectiveness associated with various combinations of inboard, outboard, and full span wing trailing edge controls. The test was conducted over a Mach number range from 0.6 to 1.08 at angles of attack from -2 deg to 23 deg at 0 deg sideslip.

“NASA Technical Reports Server (NTRS) 19770013202: Transonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC 8-foot Transonic Wind Tunnel (LA48)” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 19770013202: Transonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC 8-foot Transonic Wind Tunnel (LA48)
  • Author: ➤  
  • Language: English

“NASA Technical Reports Server (NTRS) 19770013202: Transonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC 8-foot Transonic Wind Tunnel (LA48)” Subjects and Themes:

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Downloads Information:

The book is available for download in "texts" format, the size of the file-s is: 165.44 Mbs, the file-s for this book were downloaded 74 times, the file-s went public at Tue Jul 26 2016.

Available formats:
Abbyy GZ - Animated GIF - Archive BitTorrent - DjVuTXT - Djvu XML - Item Tile - Metadata - Scandata - Single Page Processed JP2 ZIP - Text PDF -

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Find NASA Technical Reports Server (NTRS) 19770013202: Transonic Control Effectiveness For Full And Partial Span Elevon Configurations On A 0.0165 Scale Model Space Shuttle Orbiter Tested In The LaRC 8-foot Transonic Wind Tunnel (LA48) at online marketplaces:


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