NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration - Info and Reading Options
By NASA Technical Reports Server (NTRS)
"NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration" and the language of the book is English.
“NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration” Metadata:
- Title: ➤ NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration
- Author: ➤ NASA Technical Reports Server (NTRS)
- Language: English
Edition Identifiers:
- Internet Archive ID: NASA_NTRS_Archive_20160009102
AI-generated Review of “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration”:
"NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration" Description:
The Internet Archive:
A high fidelity aeroacoustic test was conducted in the NASA Langley 14- by 22-Foot Subsonic Tunnel to establish a detailed database of component noise for a 5.8% scale HWB aircraft configuration. The model has a modular design, which includes a drooped and a stowed wing leading edge, deflectable elevons, twin verticals, and a landing gear system with geometrically scaled wheel-wells. The model is mounted inverted in the test section and noise measurements are acquired at different streamwise stations from an overhead microphone phased array and from overhead and sideline microphones. Noise source distribution maps and component noise spectra are presented for airframe configurations representing two different approach flight conditions. Array measurements performed along the aircraft flyover line show the main landing gear to be the dominant contributor to the total airframe noise, followed by the nose gear, the inboard side-edges of the LE droop, the wing tip/LE droop outboard side-edges, and the side-edges of deployed elevons. Velocity dependence and flyover directivity are presented for the main noise components. Decorrelation effects from turbulence scattering on spectral levels measured with the microphone phased array are discussed. Finally, noise directivity maps obtained from the overhead and sideline microphone measurements for the landing gear system are provided for a broad range of observer locations.
Read “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration”:
Read “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration” by choosing from the options below.
Available Downloads for “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration”:
"NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration" is available for download from The Internet Archive in "texts" format, the size of the file-s is: 2.03 Mbs, and the file-s went public at Tue Jan 12 2021.
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
- All Files are Available: Yes
- Number of Files: 5
- Number of Available Files: 5
- Added Date: 2021-01-12 22:31:39
- Scanner: Internet Archive Python library 1.9.6
Available Files:
1- Text PDF
- File origin: original
- File Format: Text PDF
- File Size: 0.00 Mbs
- File Name: 20160009102.pdf
- Direct Link: Click here
2- Metadata
- File origin: original
- File Format: Metadata
- File Size: 0.00 Mbs
- File Name: NASA_NTRS_Archive_20160009102_files.xml
- Direct Link: Click here
3- Metadata
- File origin: original
- File Format: Metadata
- File Size: 0.00 Mbs
- File Name: NASA_NTRS_Archive_20160009102_meta.sqlite
- Direct Link: Click here
4- Metadata
- File origin: original
- File Format: Metadata
- File Size: 0.00 Mbs
- File Name: NASA_NTRS_Archive_20160009102_meta.xml
- Direct Link: Click here
5- Archive BitTorrent
- File origin: metadata
- File Format: Archive BitTorrent
- File Size: 0.00 Mbs
- File Name: NASA_NTRS_Archive_20160009102_archive.torrent
- Direct Link: Click here
Search for “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration” downloads:
Visit our Downloads Search page to see if downloads are available.
Find “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration” in Libraries Near You:
Read or borrow “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration” from your local library.
Buy “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration” online:
Shop for “NASA Technical Reports Server (NTRS) 20160009102: Airframe Noise From A Hybrid Wing Body Aircraft Configuration” on popular online marketplaces.
- Ebay: New and used books.