An analytical method for predicting the stability and control characteristics of large elastic airplanes at subsonic and supersonic speeds. Part 1 - Analysis. Part 2 - Application

التفاصيل البيبلوغرافية
العنوان: An analytical method for predicting the stability and control characteristics of large elastic airplanes at subsonic and supersonic speeds. Part 1 - Analysis. Part 2 - Application
المؤلفون: Chevalier, H. L, Dornfield, G. M, Dusto, A. R, Schwanz, R. C
المصدر: AGARD AEROELASTIC EFFECTS FROM A FLIGHT MECH. STANDPOINT MAR. 1970 (SEE N70-29401 15-02).
بيانات النشر: United States: NASA Center for Aerospace Information (CASI), 1970.
سنة النشر: 1970
مصطلحات موضوعية: Aircraft
الوصف: Analytical method for predicting stability and control characteristics of large elastic airplanes at subsonic and supersonic speeds
نوع الوثيقة: Report
اللغة: English
URL الوصول: https://ntrs.nasa.gov/citations/19700020102
رقم الانضمام: edsnas.19700020102
قاعدة البيانات: NASA Technical Reports