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121113s1958 dcua b f000 0 eng d |
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‡a(MiU)990128620410106381
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‡aNACA
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‡aY 3.N21/5:15/L57J28a
|
100 |
1 |
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‡aFournier, Roger H.
|
245 |
1 |
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‡aInvestigation of the static lateral stability and aileron characteristics of a 0.067-scale model of the Bell X-2 airplane at Mach number of 2.29, 2.78, 3.22, and 3.71 /
‡cBy Roger H. Fournier and H. Norman Silvers.
|
260 |
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‡aWashington, D.C. :
‡bNational Advisory Committee for Aeronautics,
‡c1958.
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300 |
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‡a50 p. :
‡bill. ;
‡c27 cm.
|
490 |
0 |
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‡aNational Advisory Committee for Aeronautics research memorandum ;
‡vL57J28a
|
500 |
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‡a"March 3, 1958."
|
504 |
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⊔ |
‡aIncludes bibliographical references (p. 9).
|
538 |
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‡aMode of access: Internet.
|
650 |
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0 |
‡aStability of airplanes, Lateral.
|
650 |
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0 |
‡aAilerons.
|
650 |
⊔ |
0 |
‡aBell aircraft.
|
700 |
1 |
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‡aSilvers, H. Norman.
|
710 |
2 |
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‡aLangley Aeronautical Laboratory.
|
710 |
2 |
⊔ |
‡aUnited States.
‡bNational Adviosry Committee for Aeronautics.
‡tNACA research memorandum.
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730 |
0 |
⊔ |
‡aTechnical Report Archive & Image Library (TRAIL)
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‡a39015086466243
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‡b2024-03-16T17:39:44Z
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