Flight Handbook, USAF Series C-47/C47A Aircraft , Navy Model R4D-1/R4D-5 Aircraft
Title | Flight Handbook, USAF Series C-47/C47A Aircraft , Navy Model R4D-1/R4D-5 Aircraft PDF eBook |
Author | |
Publisher | |
Pages | 254 |
Release | 1957 |
Genre | Douglas DC-3 (Transport plane) |
ISBN |
Download Flight Handbook, USAF Series C-47/C47A Aircraft , Navy Model R4D-1/R4D-5 Aircraft Book in PDF, Epub and Kindle
Flight Manual
Title | Flight Manual PDF eBook |
Author | |
Publisher | |
Pages | |
Release | 1961 |
Genre | Douglas DC-3 (Transport plane) |
ISBN |
Download Flight Manual Book in PDF, Epub and Kindle
Flight Manual
Title | Flight Manual PDF eBook |
Author | United States. Air Force |
Publisher | |
Pages | |
Release | 1963 |
Genre | Douglas DC-3 (Transport plane) |
ISBN |
Download Flight Manual Book in PDF, Epub and Kindle
Bibliography of Scientific and Industrial Reports
Title | Bibliography of Scientific and Industrial Reports PDF eBook |
Author | |
Publisher | |
Pages | 612 |
Release | 1948 |
Genre | Science |
ISBN |
Download Bibliography of Scientific and Industrial Reports Book in PDF, Epub and Kindle
A Method for Measuring the Product of Inertia and the Inclination of the Principal Longitudinal Axis of Inertia of an Airplane
Title | A Method for Measuring the Product of Inertia and the Inclination of the Principal Longitudinal Axis of Inertia of an Airplane PDF eBook |
Author | Robert W. Boucher |
Publisher | |
Pages | 718 |
Release | 1954 |
Genre | Airplanes |
ISBN |
Download A Method for Measuring the Product of Inertia and the Inclination of the Principal Longitudinal Axis of Inertia of an Airplane Book in PDF, Epub and Kindle
The angle of inclination of the principal axis was found to have probable error of plus or minus 0.17 degrees both from analysis of the error of inertia measurement of the full-scale airplane and from tests with a model having a simple configuration. Analysis showed the probable error of the inertia measurements for the test airplane to be plus or minus1.00, plus or minus 0.49, and plus or minus 0.35 percent of the true moment of inertia about the X, Y, and Z body reference axes, respectively.
Technical Note
Title | Technical Note PDF eBook |
Author | |
Publisher | |
Pages | 404 |
Release | 1954 |
Genre | Aeronautics |
ISBN |
Download Technical Note Book in PDF, Epub and Kindle
Technical Note - National Advisory Committee for Aeronautics
Title | Technical Note - National Advisory Committee for Aeronautics PDF eBook |
Author | United States. National Advisory Committee for Aeronautics |
Publisher | |
Pages | 412 |
Release | 1953 |
Genre | Aeronautics |
ISBN |
Download Technical Note - National Advisory Committee for Aeronautics Book in PDF, Epub and Kindle