Explore: Wind Tunnel Stability Tests
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Books Results
Source: The Open Library
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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.
- Ebay: New & used books.
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.