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Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20° to 90° / prepared for Langley Research Center (NASA contractor report ; 3248)
Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 20° to 90° / prepared for Langley Research Center (NASA contractor report ; 3248)
Microform
図書
1984
<YCA-NAS 1.26:3248>
National Diet Library
Author Heading
Ralston, J. N
Barnhart, Billy Langley Resea...
Rotary Balance Data and Analysis for the X-29A Airplane for an Angle-of-Attack Range of 0 Deg to 90 Deg NASA-CR-3747 N87-10837 NAS-1263747
Rotary Balance Data and Analysis for the X-29A Airplane for an Angle-of-Attack Range of 0 Deg to 90 Deg NASA-CR-3747 N87-10837 NAS-1263747
Microform
規格・テクニカルリポート類
Ralston, J. N
<LS-N87/10837>
National Diet Library
Rotary Balance Data for a Typical Single-Engine General Aviation Design for an Angle-of-Attack Range of 20 to 90 Deg. 3: Influence of Control Deflection on Predicted Model D Spin Modes NASA-CR-3248 N84-25641 NAS-1263248
Rotary Balance Data for a Typical Single-Engine General Aviation Design for an Angle-of-Attack Range of 20 to 90 Deg. 3: Influence of Control Deflection on Predicted Model D Spin Modes NASA-CR-3248 N84-25641 NAS-1263248
Microform
規格・テクニカルリポート類
Ralston, J. N
, Barnhart, B. P
<LS-N84/25641>
National Diet Library
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