The Development And Evaluation Of The Cal Air Force Dynamic Wind Tunnel Testing System PDF Download
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Author | : Irving C. Statler |
Publisher | : |
Total Pages | : 40 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download The Development and Evaluation of the Cal/air Force Dynamic Wind-tunnel Testing System Book in PDF, ePub and Kindle
Author | : Irving C. Statler |
Publisher | : |
Total Pages | : 44 |
Release | : 1967 |
Genre | : |
ISBN | : |
Download The Development and Evaluation of the Cal/air Force Dynamic Wind-tunnel Testing System. Part Ii. Dynamic Tests of an F-104 Model Book in PDF, ePub and Kindle
The F-104 model was designed and fabricated by the Air Force Flight Dynamics Laboratory and incorporated an unusual force and motion sensing system utilizing an internal dummy model with duplicate mass, inertia, and c.g. location. Longitudinal dynamic tests were performed with this model up through the transonic speed range. The results are evaluated with respect to the operation of the dynamic testing system and to the performance of the dummy model for measuring motion and canceling inertial loads. (Author).
Author | : Irving C. Statler |
Publisher | : |
Total Pages | : 60 |
Release | : 1967 |
Genre | : Wind tunnels |
ISBN | : |
Download The Development and Evaluation of the CAL/Air Force Dynamic Wind- Tunnel Testing System: Dynamic tests of an F-104 model Book in PDF, ePub and Kindle
Author | : Irving C. Statler |
Publisher | : |
Total Pages | : 172 |
Release | : 1967 |
Genre | : Wind tunnels |
ISBN | : |
Download The Development and Evaluation of the CAL/Air Force Dynamic Wind- Tunnel Testing System: Description and dynamic tests of an F-80 model [by] Irving C. Statler, Orren B. Tufts [and] Walter J. Hirtreiter Book in PDF, ePub and Kindle
Author | : Irving C. Statler |
Publisher | : |
Total Pages | : 153 |
Release | : 1967 |
Genre | : Airplanes |
ISBN | : |
Download The Development and Evaluation of the CAL/Air Force Dynamic Wind-tunnel Testing System Book in PDF, ePub and Kindle
The Cornell Aeronautical Laboratory (CAL) system provides a unique mounting through which a model can be forced precisely in any desired planar sinusoidal motion. The versatility and overall accuracy of the CAL/Air Force dynamic testing system was demonstrated during a series of wind-tunnel tests. These tests permitted, for the first time, a measurement of the separate components of the rotary damping moment. The moment due to rate of change of angle of attack was measured by oscillating the model in pure plunging motion. The moment due to pitch rate was measured during pitching motion. The sum of these is compared with the total rotary damping moment as measured in rotation. Comparisons of data taken at two frequencies and four Mach numbers indicate that the components are accurate to within plus or minus ten percent of the total rotary damping moment. The results are compared with theory, flight test data, and other wind-tunnel measurements on the same and similar models. Future applications of this equipment are reviewed, particularly with regard to its use as a research tool to support basic investigations for the development of theoretical or semiempirical methods for predicting dynamic stability characteristics of aircraft at transonic speeds. (Author).
Author | : Irving C. Statler |
Publisher | : |
Total Pages | : 32 |
Release | : 1967 |
Genre | : Airplanes |
ISBN | : |
Download The Development and Evaluation of the CAL/Air Force Dynamic Wind-tunnel Testing System Book in PDF, ePub and Kindle
The F-104 model was designed and fabricated by the Air Force Flight Dynamics Laboratory and incorporated an unusual force and motion sensing system utilizing an internal dummy model with duplicate mass, inertia, and c.g. location. Longitudinal dynamic tests were performed with this model up through the transonic speed range. The results are evaluated with respect to the operation of the dynamic testing system and to the performance of the dummy model for measuring motion and canceling inertial loads.
Author | : |
Publisher | : |
Total Pages | : 1470 |
Release | : 1967-05 |
Genre | : Government publications |
ISBN | : |
Download Government-wide Index to Federal Research & Development Reports Book in PDF, ePub and Kindle
Author | : |
Publisher | : |
Total Pages | : 1572 |
Release | : 1992 |
Genre | : Aeronautics |
ISBN | : |
Download Scientific and Technical Aerospace Reports Book in PDF, ePub and Kindle
Author | : Defense Documentation Center (U.S.) |
Publisher | : |
Total Pages | : 784 |
Release | : 1967 |
Genre | : Science |
ISBN | : |
Download Technical Abstract Bulletin Book in PDF, ePub and Kindle
Author | : H. Daughaday |
Publisher | : |
Total Pages | : 66 |
Release | : 1957 |
Genre | : Aeronautics |
ISBN | : |
Download Measurement of Dynamic Stability Derivatives in the Wind Tunnel Book in PDF, ePub and Kindle