Author: John BosharPublisher:
ISBN:
Category :
Languages : en
Pages : 21
Book Description
Some Flight Measurement of Pressure Distribution During Tail Buffeting
Author: John BosharPublisher:
ISBN:
Category :
Languages : en
Pages : 21
Book Description
Some Flight Measurements of Pressure Distribution During Tail Buffeting
Author: John BosharPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22
Book Description
Results are presented of pressure-distribution measurements taken over the horizontal tail surfaces of a Curtiss P-40K airplane during several low-speed pull-ups to abrupt stall in which tail buffeting was experienced.
Flight Studies of the Horizontal-tail Loads Experienced by a Modern Pursuit Airplane in Abrupt Maneuvers
Author: Langley Aeronautical LaboratoryPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 50
Book Description
Summary: Flight measurements were made on a modern pursuit airplane to determine the approximate magnitude of the horizontal tail loads in accelerated flight. In these flight measurements, pressures at a few points were used as an index of the tail loads by correlating these pressures with complete pressure-distribution data obtained in the NACA full-scale tunnel. In addition, strain gages and motion pictures of tail deflections were used to explore the general nature and order of magnitude of the fluctuating tail loads in accelerated stalls. The results indicated that, if the airplane were not stalled, a total up load of 5700 pounds would be experienced on the horizontal tail in an 8g pull-up and that, with power on, this load would be distributed unsymmetrically with about 800 pounds more up load on the left stabilizer than on the right. When stalling occurred there was an initial abrupt increase in the up tail load of the order of 100 percent of the previous load, which was followed by repeated load and stress variations due to tail buffeting. Under the condition of tail buffeting, the possibility of excessive stresses due to resonance was indicated.
NACA Wartime Report
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 716
Book Description
Wartime Report
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 622
Book Description
Reproductions of reports, some declassified, of research done at Langley Memorial Aeronautical Laboratory during World War II. The order of reports does not represent when they were chronologically issued. Reference to the original version of each report is included.
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
Wartime Report
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 440
Book Description
Flight Studies of the Horizontal-tail Loads Experienced by a Fighter Airplane in Abrupt Maneuvers
Author: Langley Aeronautical LaboratoryPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 16
Book Description
Flight measurements were made on a fighter airplane to determine the approximate magnitude of the horizontal tail loads in accelerated flight. In these flight measurements, pressures at a few points were used as an index of the tail loads by correlating these pressures with complete pressure-distribution data obtained in the NACA full-scale tunnel. In addition, strain gages and motion pictures of tail deflections were used to explore the general nature and order of magnitude of the fluctuating tail loads in accelerated stalls. The results indicated that, if the airplane were not stalled, a total up load of 5700 pounds would be experienced on the horizontal tail in an 8g pull-up and that, with power on, this load would be distributed unsymmetrically with about 800 pounds more up load on the left stabilizer than on the right. When stalling occurred there was an initial abrupt increase in the up tail load of the order of 100 percent of the previous load, which was followed by repeated load and stress variations due to tail buffeting. Under the condition of tail buffeting, the possibility of excessive stresses due to resonance was indicated.
Analytical Method of Determining Transmission of Particles and Radiation Through Great Thickness of Matter
Author: A. R. BobrowskyPublisher:
ISBN:
Category : Mathematical analysis
Languages : en
Pages : 668
Book Description
A matrixc method of determining transmission, scattering, and absorption of radition, such as gamma rays and neutrons, is presented in this report.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 816
Book Description
