Effects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degrees sweptback surfaces with some reference to mutual interference /
Results are presented of an investigation made to determine the effects of wing position and horizontal-tail position on the low-speed static static lateral and static longitudinal stability characteristics of airplane models having unswept and 45 degree sweptback surfaces. Interference increments b...
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| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1951
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2504 |
| Subjects: | |
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| LEADER | 02236nam a2200349Ia 4500 | ||
|---|---|---|---|
| 001 | 116d0ad3-4f9e-4900-a6f0-496466f90979 | ||
| 005 | 20230617000000.0 | ||
| 008 | 100924e195110 dcua tb f000 0 eng d | ||
| 035 | |a (OCoLC-I)795636050 | ||
| 035 | |a (OCoLC-M)665167608 | ||
| 040 | |a LHL |c LHL |d LHL |d CSt |d UtOrBLW | ||
| 086 | 0 | |a Y 3.N 21/5:6/2504 | |
| 100 | 1 | |a Goodman, Alex | |
| 245 | 1 | 0 | |a Effects of wing position and horizontal-tail position on the static stability characteristics of models with unswept and 45 degrees sweptback surfaces with some reference to mutual interference / |c Alex Goodman |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1951 | ||
| 300 | |a 58 p. : |b ill ; |c 28 cm | ||
| 490 | 1 | |a National Advisory Committee for Aeronautics ; |v no. 2504 | |
| 500 | |a NACA TN No. 2504 | ||
| 500 | |a "October 1951." | ||
| 504 | |a Includes bibliographical references | ||
| 520 | 3 | |a Results are presented of an investigation made to determine the effects of wing position and horizontal-tail position on the low-speed static static lateral and static longitudinal stability characteristics of airplane models having unswept and 45 degree sweptback surfaces. Interference increments between the various components are evaluated, and efficiency factors of the vertical tail as a function of wing position are presented | |
| 590 | |a Copy 1 bound with 2491 |c 9122747 (parent record's ckey) |b 36105024831211 (item id) | ||
| 596 | |a 31 | ||
| 650 | 0 | |a Airplanes |x Models |x Wings | |
| 650 | 0 | |a Airplanes |x Tail surfaces | |
| 650 | 0 | |a Interference (Aerodynamics) | |
| 650 | 0 | |a Stability of airplanes, Lateral | |
| 650 | 0 | |a Stability of airplanes, Longitudinal | |
| 710 | 1 | |a United States |b National Advisory Committee for Aeronautics. | |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 2504 | |
| 999 | 1 | 0 | |i 116d0ad3-4f9e-4900-a6f0-496466f90979 |l a9122776 |s US-CST |m effects_of_wing_position_and_horizontal_tail_position_on_the_static_st_____1951_______natioa________________________________________goodman__alex______________________y_3_n_21_5_6_2504p |
| 999 | 1 | 1 | |l a9122776 |s ISIL:US-CST |t BKS |a SAL3 SEE-OTHER |b 9122776-1001 |c NACA TN 2504 |d ALPHANUM |x STKS-MONO |y 9122776-1001 |p UNLOANABLE |