Explore: Wind Tunnel Stability Tests
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
By David E. Hahne
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Metadata:
- Title: ➤ Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept
- Author: David E. Hahne
- Language: English
- Number of Pages: Median: 23
- Publisher: ➤ Available from the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Springfield, VA - Hampton, Va
“Evaluation of the low-speed stability and control characteristics of a Mach 5.5 waverider concept” Subjects and Themes:
- Subjects: ➤ Aerodynamic characteristics - Aerodynamic coefficients - Aerodynamic stability - Aerodynamics, Hypersonic - Angle of attack - Hypersonic Aerodynamics - Hypersonic speed - Hypersonic vehicles - Low speed - Mach number - Pitching moments - Stability - Stability of airplanes - Stabilizers (Fluid dynamics) - Vortices - Waveriders - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL18134999M - OL17133262M - OL17839424M - OL21033491M - OL15549003M
- Online Computer Library Center (OCLC) ID: 42055832
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
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2Full-scale hingeless rotor performance and loads
By Randall L. Peterson
“Full-scale hingeless rotor performance and loads” Metadata:
- Title: ➤ Full-scale hingeless rotor performance and loads
- Author: Randall L. Peterson
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ Moffett Field, Calif - [Springfield, Va
“Full-scale hingeless rotor performance and loads” Subjects and Themes:
- Subjects: ➤ 80-105 helicopter - Aerodynamic loads - Aerodynamic stability - Aeroelasticity - Data bases - Databases - Full scale tests - Rigid rotors - Rotating shafts - Rotor aerodynamics - Rotor blades - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL17070226M - OL17117614M - OL18086109M - OL15421543M
- Online Computer Library Center (OCLC) ID: 35216887
Access and General Info:
- First Year Published: 1995
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Full-scale hingeless rotor performance and loads at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
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3Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
By Bobby W. Sanders
“Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” Metadata:
- Title: ➤ Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
- Author: Bobby W. Sanders
- Language: English
- Number of Pages: Median: 98
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1980
- Publish Location: Washington, D.C
“Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients” Subjects and Themes:
- Subjects: ➤ Airplanes - Turbojet engines - Air intakes - Motors - Valves - Aerodynamic stability - Bypasses - Propulsion system performance - Supersonic inlets - Wind tunnel stability tests
Edition Identifiers:
- The Open Library ID: OL43506459M
- Online Computer Library Center (OCLC) ID: 761221787
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
List of wind tunnels
This is an alphabetical list of wind tunnels. "A2 wind tunnel". Retrieved 26 January 2024. "ACE Climatic Wind Tunnel". Retrieved 26 January 2024. "Fly
Virginia Tech Stability Wind Tunnel
The Virginia Tech Stability Wind Tunnel is a medium-scale wind tunnel located at Virginia Polytechnic Institute and State University (Virginia Tech) in
Long Range – Anti Ship Missile (India)
Minister Rajnath Singh formally inaugurated the ₹400 crore, Hypersonic Wind Tunnel (HWT) test facility at the Dr. A. P. J. Abdul Kalam Missile Complex. With a
Lockheed Martin X-59 Quesst
vision system (XVS) was flight tested on a King Air at NASA Langley. This is to be followed by high speed wind tunnel tests to verify inlet performance predictions
Robert Thomas Jones (engineer)
Aeronautics, Jan. 1974 With Smith, R., and Summers, J., Transonic Wind Tunnel Tests of an F-8 Airplane Model Equipped with 12 and 14-percent Thick Oblique
Boom XB-1
through three sets of wind tunnel tests. The first indicated that the predicted calibration was off by 30%. The second set of tests confirmed accurate calibration
Douglas D-558-2 Skyrocket
pitch-up conditions, leading edge chord extensions did not, disproving wind-tunnel tests to the contrary. Slats (long, narrow auxiliary airfoils) in the fully
Wright Flyer
efficient wings and propellers, which resulted from the Wrights' exacting wind tunnel tests and made the most of the marginal power delivered by their early homebuilt
Ames Research Center
personnel and a US$750 million annual budget. Ames was founded to conduct wind-tunnel research on the aerodynamics of propeller-driven aircraft; however, its
Bell Boeing Quad TiltRotor
V-22. A one-fifth-scale wind tunnel model has undergone testing in the Transonic Dynamics Tunnel (a unique transonic wind tunnel) at NASA's Langley Research