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NACA-WR-L-704
Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons
Year: 1942
Abstract: INTRODUCITON
At the request of the Material Command, Army air Forces, tests were made in the Langley two-dimensional tunnel of four models submitted by the Glenn L, Martin Company as intermediate sections of the wing of the XB-33 airplane. The models were of 24-inch chord and were constructed of wood with pressure-distribution crifices. the models were identified by station numbers of 85, 250, 430, and 620, respectively, of the wing of the XB-33 airplane. This wing is formed by fairing between an NACA 65,2-222 a = 1 root section and an NACA 65,2-415 a = 0.5 tip section.
Sections number 85 and 430 were represented by simple airfoil models without flaps.
At the request of the Material Command, Army air Forces, tests were made in the Langley two-dimensional tunnel of four models submitted by the Glenn L, Martin Company as intermediate sections of the wing of the XB-33 airplane. The models were of 24-inch chord and were constructed of wood with pressure-distribution crifices. the models were identified by station numbers of 85, 250, 430, and 620, respectively, of the wing of the XB-33 airplane. This wing is formed by fairing between an NACA 65,2-222 a = 1 root section and an NACA 65,2-415 a = 0.5 tip section.
Sections number 85 and 430 were represented by simple airfoil models without flaps.
Subject: AILERONS
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:38:42Z | |
| date available | 2017-09-04T16:38:42Z | |
| date copyright | 01/01/1942 | |
| date issued | 1942 | |
| identifier other | VJCZYDAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/102305 | |
| description abstract | INTRODUCITON At the request of the Material Command, Army air Forces, tests were made in the Langley two-dimensional tunnel of four models submitted by the Glenn L, Martin Company as intermediate sections of the wing of the XB-33 airplane. The models were of 24-inch chord and were constructed of wood with pressure-distribution crifices. the models were identified by station numbers of 85, 250, 430, and 620, respectively, of the wing of the XB-33 airplane. This wing is formed by fairing between an NACA 65,2-222 a = 1 root section and an NACA 65,2-415 a = 0.5 tip section. Sections number 85 and 430 were represented by simple airfoil models without flaps. | |
| language | English | |
| title | NACA-WR-L-704 | num |
| title | Tests of four models representing intermediate sections of the XB-33 airplane including sections with slotted flap and ailerons | en |
| type | standard | |
| page | 30 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1942 | |
| contenttype | fulltext | |
| subject keywords | AILERONS | |
| subject keywords | AIRFOILS | |
| subject keywords | BALANCED | |
| subject keywords | BRISTOL | |
| subject keywords | CHAR | |
| subject keywords | DEFLECTION | |
| subject keywords | DIM | |
| subject keywords | DISTRIBUTION | |
| subject keywords | DRAG | |
| subject keywords | FLAPS | |
| subject keywords | FRISE | |
| subject keywords | HINGE | |
| subject keywords | LOW | |
| subject keywords | MARTIN | |
| subject keywords | MOMENTS | |
| subject keywords | NACA | |
| subject keywords | PRESSURE | |
| subject keywords | SLOTTED | |
| subject keywords | TESTS | |
| subject keywords | TUNNEL | |
| subject keywords | WIND | |
| subject keywords | WING | |
| subject keywords | WINGS |