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Theoretical stability derivatives for the x-15 research airplane at supersonic and hypersonic speeds including a comparison with wind-tunnel results

机译：x-15研究飞机在超音速和高超音速下的理论稳定性导数，包括与风洞结果的比较

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摘要

Longitudinal and lateral stability and control derivatives for X-15A aircraft at supersonic and hypersonic speeds - comparison of theoretical results with wind tunnel testing

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作者
Walker, H. J.; Wolowicz, C. H.;
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年度 1960
页码 1-116
总页数 116
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
DERIVATION; HYPERSONIC SPEED; LATERAL CONTROL; LATERAL STABILITY; LONGITUDINAL CONTROL; LONGITUDINAL STABILITY; STABILITY DERIVATIVES; SUPERSONIC SPEED; WIND TUNNEL TESTS; WIND TUNNELS; X-15 AIRCRAFT; HYPERSONIC SPEED; LATERAL STABILITY AND CONTROL; LONGITUDINAL STABILITY AND CONTROL; SUPERSONIC SPEED; X-15 AIRCRAFT;

机译：推导;超速的;横向控制;横向稳定性;纵向控制;纵向稳定性;稳定性衍生物;超音速;风洞隧道测试;风洞; X-15飞机;超速的;横向稳定性和控制;纵向稳定性和控制;超音速; X-15飞机;

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2. Unsteady Unified Hypersonic/Supersonic Method for Aeroelastic Applications Including Wave/Shock Interaction [J] . Frank R. Chavez, D. D. Liu AIAA Journal . 1995 ,第6期

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3. Definition system and criteria related to the static stability of airplanes (first report) -definition system, static flight speed stability, and static angle of attack stability- [J] . osamu Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2002 ,第148期

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5. Determination of stability and control derivatives for a modern light composite twin engine airplane. [D] . Londono, Monica M. 2009

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6. The Influence of pH and Temperature on the Stability of N-(Piperidine)methylenedaunorubicin Hydrochloride and a Comparison of the Stability of Daunorubicin and Its Four New Amidine Derivatives in Aqueous Solutions [O] . Mikołaj Piekarski, Agnieszka Dołhań, Judyta Cielecka-Piontek, -1

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7. A study of the longitudinal low frequency (phugoid) motion of an airplane at supersonic and hypersonic speeds [O] . Walter Uso 1967

机译：研究飞机在超音速和高超音速下的纵向低频（phugoid）运动

Theoretical stability derivatives for the x-15 research airplane at supersonic and hypersonic speeds including a comparison with wind-tunnel results

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