Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces /
This report contains wind-tunnel results of the effect of change in horizontal-tail size and location on the static-lateral-stability parameters for a complete mode with wing and tail surfaces having the quarter-chord line swept back 45 degrees. Charts applicable to the design of similar tail config...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2010 |
| Subjects: | |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| LEADER | 02284nam a2200385Ia 4500 | ||
|---|---|---|---|
| 001 | ccb8985c-41cd-4934-98b1-dd454d4eabc6 | ||
| 005 | 20240926000000.0 | ||
| 008 | 100907e195001 dcua tb f000 0 eng d | ||
| 035 | |a (OCoLC-I)793497726 | ||
| 035 | |a (OCoLC-M)662494589 | ||
| 035 | |a (Sirsi) o662494589 | ||
| 035 | |a (Sirsi) ocn662494589 | ||
| 040 | |a LHL |c LHL |d LHL |d CSt |d UtOrBLW | ||
| 086 | 0 | |a Y 3.N 21/5:6/2010 | |
| 100 | 1 | |a Brewer, Jack D | |
| 245 | 1 | 0 | |a Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces / |c Jack D. Brewer and Jacob H. Lichtenstein |
| 260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1950 | ||
| 300 | |a 46 p. : |b ill ; |c 28 cm | ||
| 490 | 1 | |a National Advisory Committee for Aeronautics ; |v no. 2010 | |
| 500 | |a NACA TN No. 2010 | ||
| 500 | |a "January 1950." | ||
| 504 | |a Includes bibliographical references | ||
| 520 | 3 | |a This report contains wind-tunnel results of the effect of change in horizontal-tail size and location on the static-lateral-stability parameters for a complete mode with wing and tail surfaces having the quarter-chord line swept back 45 degrees. Charts applicable to the design of similar tail configurations are included | |
| 590 | |a Copy 1 bound with 2002 |c 9122616 (parent record's ckey) |b 36105024795945 (item id) | ||
| 650 | 0 | |a Airplanes |x Models |x Testing | |
| 650 | 0 | |a Airplanes |x Tail surfaces | |
| 650 | 0 | |a Airplanes |x Wings, Swept-back | |
| 650 | 0 | |a Stability of airplanes, Lateral | |
| 650 | 0 | |a Wind tunnel testing | |
| 700 | 1 | |a Lichtenstein, Jacob H | |
| 710 | 1 | |a United States |b National Advisory Committee for Aeronautics. | |
| 830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 2010 | |
| 999 | 1 | 0 | |i ccb8985c-41cd-4934-98b1-dd454d4eabc6 |l a9122596 |s US-CST |m effect_of_horizontal_tail_on_low_speed_static_lateral_stability_charac_____1950_______natioa________________________________________brewer__jack_d_____________________y_3_n_21_5_6_2010p |
| 999 | 1 | 1 | |l a9122596 |s ISIL:US-CST |t BKS |b 3016bf83-ef79-5ca8-82e1-e2f95961a254 |y 3016bf83-ef79-5ca8-82e1-e2f95961a254 |p UNLOANABLE |
| 999 | 1 | 1 | |l a9122596 |s ISIL:US-CST |t BKS |a SAL3-SEE-OTHER |c NACA TN 2010 |d Shelving control number |p UNLOANABLE |