Techniques For Measurement Of Dynamic Stability Derivatives In Ground Test Facilities PDF Download
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Author | : Clarence John Schueler |
Publisher | : |
Total Pages | : 242 |
Release | : 1967 |
Genre | : Aerodynamic measurements |
ISBN | : |
Download Techniques for Measurement of Dynamic Stability Derivatives in Ground Test Facilities Book in PDF, ePub and Kindle
Some of the techniques in current use for measuring dynamic stability derivatives in wind tunnels are described, with emphasis given to the important features of balance system design, data reduction methods, instrumentation and typical balance systems. The use of gas bearings for dynamic stability and roll damping balances is treated and a three-degree-of-freedom balance system employing a spherical gas bearing is described. (Author).
Author | : C.J. Schueler |
Publisher | : |
Total Pages | : |
Release | : 1967 |
Genre | : |
ISBN | : |
Download Techniques for Measurements of Dynamic Stability Derivates in Fround Test Facilities Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 702 |
Release | : 1995 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : Bandu N. Pamadi |
Publisher | : AIAA |
Total Pages | : 810 |
Release | : 2004 |
Genre | : Aerodynamics |
ISBN | : 9781600860997 |
Download Performance, Stability, Dynamics, and Control of Airplanes Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 296 |
Release | : 1991 |
Genre | : Aeronautics |
ISBN | : |
Download NASA Technical Memorandum Book in PDF, ePub and Kindle
Author | : Frederick B. Cyran |
Publisher | : |
Total Pages | : 58 |
Release | : 1981 |
Genre | : Boundary layer |
ISBN | : |
Download Evaluation of Critical Sting Length on a 7-deg Cone as Determined by Measurements of Dynamic Stability Derivatives and Base Pressure for Mach Numbers 0.2 Through 1.3 Book in PDF, ePub and Kindle
Wind tunnel tests were conducted to provide sting-support interference information for planning and directing wind tunnel tests at subsonic and transonic Mach numbers. Sting-length effects on dynamic stability derivatives, static pitching moment, and base pressure of a blunt, flat-base 7- deg cone were investigated at Mach numbers 0.2 to 1.3 in the Arnold Engineering Development Center (AEDC) Propulsion Wind Tunnel Facility (PWT). Two frequencies of oscillation, nominally 5.3 and 2.9 Hz, were investigated. The boundary-layer state at the model base was turbulent for all Mach numbers greater than 0.2. The interference effects of two types of model-wake splitter plates were also investigated. The results showed that the critical sting length depended on the Mach number, angle of attack, and type of data used as the interference indicator. A critical sting length of three model diameters was determined to be suitable for all test conditions for the ratio of sting-diameter-to-model-base- diameter (0.22) for this test.
Author | : Bryan E. Richards |
Publisher | : |
Total Pages | : 360 |
Release | : 1977 |
Genre | : Science |
ISBN | : |
Download Measurement of Unsteady Fluid Dynamic Phenomena Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 746 |
Release | : 1968-07 |
Genre | : Science |
ISBN | : |
Download Bibliography of Scientific and Industrial Reports Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1000 |
Release | : 1978 |
Genre | : Monographic series |
ISBN | : |
Download Titles in Series Book in PDF, ePub and Kindle
A handbook for librarians and students.
Author | : |
Publisher | : |
Total Pages | : 786 |
Release | : 1975 |
Genre | : Aeronautics |
ISBN | : |
Download A Collection of Technical Papers Book in PDF, ePub and Kindle