"DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade" - Information and Links:

DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade - Info and Reading Options

"DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade" and the language of the book is English.


“DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade” Metadata:

  • Title: ➤  DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade
  • Author: ➤  
  • Language: English

Edition Identifiers:

  • Internet Archive ID: DTIC_ADA333407

AI-generated Review of “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade”:


"DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade" Description:

The Internet Archive:

This thesis contains a detailed experimental and numerical investigation of second-generation, controlled-diffusion, compressor-stator blades at an off-design inlet-flow angle of 39%5c Investigation of the blades took place in a low-speed cascade wind tunnel using various experimental procedures. The objective of the wind tunnel study was to characterize the flow field in and around the blades at the off-design angle, and to investigate flow separation near the mid-chord for a high Reynolds number of 640,000. Rake probe survey's were performed upstream and downstream of the blades in order to obtain spanwise total pressure profiles. Surface flow visualization was performed on the blades using a titanium dioxide and kerosene mixture. Blade surface pressure measurements were obtained using a 40-hole instrumented blade from which coefficients of pressure were calculated. A standard optics, two-component, laser-Doppler velocimeter was used to characterize the flow field upstream, in the boundary layer on the suction side of the blades, and in the wake region. A numerical investigation was conducted using the rotor viscous code 3-D developed by Dr. Roderick Chima of NASA Lewis Research Center. Overall, good agreement between flow visualization, blade pressure measurements, laser measurements, and numerical modeling was obtained.

Read “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade”:

Read “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade” by choosing from the options below.

Available Downloads for “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade”:

"DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade" is available for download from The Internet Archive in "texts" format, the size of the file-s is: 84.57 Mbs, and the file-s went public at Mon Apr 09 2018.

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: 17
  • Number of Available Files: 17
  • Added Date: 2018-04-09 07:22:09
  • PPI (Pixels Per Inch): 600

Available Files:

1- Image Container PDF

  • File origin: original
  • File Format: Image Container PDF
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407.pdf
  • Direct Link: Click here

2- Metadata

  • File origin: original
  • File Format: Metadata
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_files.xml
  • Direct Link: Click here

3- Metadata

  • File origin: original
  • File Format: Metadata
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_meta.sqlite
  • Direct Link: Click here

4- Metadata

  • File origin: original
  • File Format: Metadata
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_meta.xml
  • Direct Link: Click here

5- JPEG Thumb

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

6- Abbyy GZ

  • File origin: derivative
  • File Format: Abbyy GZ
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_abbyy.gz
  • Direct Link: Click here

7- chOCR

  • File origin: derivative
  • File Format: chOCR
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_chocr.html.gz
  • Direct Link: Click here

8- DjVuTXT

  • File origin: derivative
  • File Format: DjVuTXT
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_djvu.txt
  • Direct Link: Click here

9- Djvu XML

  • File origin: derivative
  • File Format: Djvu XML
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_djvu.xml
  • Direct Link: Click here

10- hOCR

  • File origin: derivative
  • File Format: hOCR
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_hocr.html
  • Direct Link: Click here

11- OCR Page Index

  • File origin: derivative
  • File Format: OCR Page Index
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_hocr_pageindex.json.gz
  • Direct Link: Click here

12- OCR Search Text

  • File origin: derivative
  • File Format: OCR Search Text
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_hocr_searchtext.txt.gz
  • Direct Link: Click here

13- Single Page Processed JP2 ZIP

  • File origin: derivative
  • File Format: Single Page Processed JP2 ZIP
  • File Size: 0.07 Mbs
  • File Name: DTIC_ADA333407_jp2.zip
  • Direct Link: Click here

14- Page Numbers JSON

  • File origin: derivative
  • File Format: Page Numbers JSON
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_page_numbers.json
  • Direct Link: Click here

15- Scandata

  • File origin: derivative
  • File Format: Scandata
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_scandata.xml
  • Direct Link: Click here

16- Additional Text PDF

  • File origin: derivative
  • File Format: Additional Text PDF
  • File Size: 0.01 Mbs
  • File Name: DTIC_ADA333407_text.pdf
  • Direct Link: Click here

17- Archive BitTorrent

  • File origin: metadata
  • File Format: Archive BitTorrent
  • File Size: 0.00 Mbs
  • File Name: DTIC_ADA333407_archive.torrent
  • Direct Link: Click here

Search for “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade” downloads:

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

Find “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade” in Libraries Near You:

Read or borrow “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade” from your local library.

Buy “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade” online:

Shop for “DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade” on popular online marketplaces.



Find "DTIC ADA333407: Experimental And Numerical Investigation Of Second-Generation, Controlled-Diffusion, Compressor Blades In Cascade" in Wikipdedia