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‡asdr-uiuc579107
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‡a830-H-14 (microfiche)
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‡aNAS 1.26:3246
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‡aRotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8t̊o 90 ̊/
‡cprepared for Langley Research Center.
|
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‡aWashington, D.C. :
‡bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ;
‡a[Springfield, Va. :
‡bFor sale by the National Technical Information Service],
‡c1983-
|
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‡aNASA contractor report ;
‡v3246
|
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⊔ |
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‡aChiefly graphs.
|
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⊔ |
⊔ |
‡a"March 1983"--Cover.
|
504 |
⊔ |
⊔ |
‡aIncludes bibliographical references.
|
505 |
1 |
⊔ |
‡av. 1. Influence of airplane components for model D / J. N. Ralston.
|
538 |
⊔ |
⊔ |
‡aMode of access: Internet.
|
650 |
⊔ |
0 |
‡aUnsteady flow (Aerodynamics)
|
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⊔ |
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‡aSpin (Aerodynamics)
|
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‡aWind tunnels
‡xFlow visualization
|
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‡aAirplanes
‡xWings
|
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‡aRotational motion (Rigid dynamics)
|
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‡aRalston, J. N.
|
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‡aUnited States.
‡bNational Aeronautics and Space Administration.
‡bScientific and Technical Information Branch.
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‡aLangley Research Center.
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‡tUS fed doc--NTIS: pubdate >= 2019
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