"NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators" - Information and Links:

NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators - Info and Reading Options

"NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators" and the language of the book is English.


“NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators” Metadata:

  • Title: ➤  NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators
  • Author: ➤  
  • Language: English

Edition Identifiers:

  • Internet Archive ID: NASA_NTRS_Archive_20140011412

AI-generated Review of “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators”:


"NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators" Description:

The Internet Archive:

Results are presented from a recent set of wind tunnel experiments using sweeping jet actuators to control ow separation on the 30% chord trailing edge ap of a 30 deg. swept wing model with an aspect ratio (AR) of 4.35. Two sweeping jet actuator locations were examined, one on the flap shoulder and one on the trailing edge flap. The parameters that were varied included actuator momentum, freestream velocity, and trailing edge flap deflection (Delta f ) angle. The primary focus of this set of experiments was to determine the mass flow and momentum requirements for controlling separation on the flap, especially at large flap deflection angles which would be characteristic of a high lift system. Surface pressure data, force and moment data, and stereoscopic particle image velocimetry (PIV) data were acquired to evaluate the performance benefits due to applying active flow control. Improvements in lift over the majority of the wing span were obtained using sweeping jet actuator control. High momentum coefficient, Cu, levels were needed when using the actuators on the ap because they were located downstream of separation. Actuators on the flap shoulder performed slightly better but actuator size, orientation, and spacing still need to be optimized.

Read “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators”:

Read “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators” by choosing from the options below.

Available Downloads for “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators”:

"NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators" is available for download from The Internet Archive in "texts" format, the size of the file-s is: 25.56 Mbs, and the file-s went public at Wed Nov 16 2016.

Legal and Safety Notes

Copyright Disclaimer and Liability Limitation:

A. Automated Content Display
The creation of this page is fully automated. All data, including text, images, and links, is displayed exactly as received from its original source, without any modification, alteration, or verification. We do not claim ownership of, nor assume any responsibility for, the accuracy or legality of this content.

B. Liability Disclaimer for External Content
The files provided below are solely the responsibility of their respective originators. We disclaim any and all liability, whether direct or indirect, for the content, accuracy, legality, or any other aspect of these files. By using this website, you acknowledge that we have no control over, nor endorse, the content hosted by external sources.

C. Inquiries and Disputes
For any inquiries, concerns, or issues related to the content displayed, including potential copyright claims, please contact the original source or provider of the files directly. We are not responsible for resolving any content-related disputes or claims of intellectual property infringement.

D. No Copyright Ownership
We do not claim ownership of any intellectual property contained in the files or data displayed on this website. All copyrights, trademarks, and other intellectual property rights remain the sole property of their respective owners. If you believe that content displayed on this website infringes upon your intellectual property rights, please contact the original content provider directly.

E. Fair Use Notice
Some content displayed on this website may fall under the "fair use" provisions of copyright law for purposes such as commentary, criticism, news reporting, research, or educational purposes. If you believe any content violates fair use guidelines, please reach out directly to the original source of the content for resolution.

Virus Scanning for Your Peace of Mind:

The files provided below have already been scanned for viruses by their original source. However, if you’d like to double-check before downloading, you can easily scan them yourself using the following steps:

How to scan a direct download link for viruses:

  • 1- Copy the direct link to the file you want to download (don’t open it yet).
  • (a free online tool) and paste the direct link into the provided field to start the scan.
  • 2- Visit VirusTotal (a free online tool) and paste the direct link into the provided field to start the scan.
  • 3- VirusTotal will scan the file using multiple antivirus vendors to detect any potential threats.
  • 4- Once the scan confirms the file is safe, you can proceed to download it with confidence and enjoy your content.

Available Downloads

  • Source: Internet Archive
  • Internet Archive Link: Archive.org page
  • All Files are Available: Yes
  • Number of Files: 12
  • Number of Available Files: 12
  • Added Date: 2016-11-16 13:09:11
  • PPI (Pixels Per Inch): 600
  • OCR: ABBYY FineReader 11.0

Available Files:

1- Text PDF

  • File origin: original
  • File Format: Text PDF
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412.pdf
  • Direct Link: Click here

2- Metadata

  • File origin: original
  • File Format: Metadata
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_files.xml
  • Direct Link: Click here

3- Metadata

  • File origin: original
  • File Format: Metadata
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_meta.sqlite
  • Direct Link: Click here

4- Metadata

  • File origin: original
  • File Format: Metadata
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_meta.xml
  • Direct Link: Click here

5- Item Tile

  • File origin: original
  • File Format: Item Tile
  • File Size: 0.00 Mbs
  • File Name: __ia_thumb.jpg
  • Direct Link: Click here

6- Animated GIF

  • File origin: derivative
  • File Format: Animated GIF
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412.gif
  • Direct Link: Click here

7- Abbyy GZ

  • File origin: derivative
  • File Format: Abbyy GZ
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_abbyy.gz
  • Direct Link: Click here

8- DjVuTXT

  • File origin: derivative
  • File Format: DjVuTXT
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_djvu.txt
  • Direct Link: Click here

9- Djvu XML

  • File origin: derivative
  • File Format: Djvu XML
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_djvu.xml
  • Direct Link: Click here

10- Single Page Processed JP2 ZIP

  • File origin: derivative
  • File Format: Single Page Processed JP2 ZIP
  • File Size: 0.02 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_jp2.zip
  • Direct Link: Click here

11- Scandata

  • File origin: derivative
  • File Format: Scandata
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_scandata.xml
  • Direct Link: Click here

12- Archive BitTorrent

  • File origin: metadata
  • File Format: Archive BitTorrent
  • File Size: 0.00 Mbs
  • File Name: NASA_NTRS_Archive_20140011412_archive.torrent
  • Direct Link: Click here

Search for “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators” downloads:

Visit our Downloads Search page to see if downloads are available.

Find “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators” in Libraries Near You:

Read or borrow “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators” from your local library.

Buy “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators” online:

Shop for “NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators” on popular online marketplaces.



Find "NASA Technical Reports Server (NTRS) 20140011412: Active Flow Separation Control On A NACA 0015 Wing Using Fluidic Actuators" in Wikipdedia