Download or read book Experimental and predicted longitudinal and lateral directional response characteristics of a large flexible 35 degree swept wing airplane at an altitude of 35 000 feet written by Henry A. Cole and published by . This book was released on 1957 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental and Predicted Longitudinal and Lateral directional Response Characteristics of a Large Flexible 35 Swept wing Airplane at an Altitude of 35 000 Feet written by Clarence A. Syvertson and published by . This book was released on 1957 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental and Predicted Longitudinal Response Characteristics of a Large Flexible 35 Degree Swept wing Airplane at an Altitude of 35 000 Feet written by Henry A. Cole (Jr.) and published by . This book was released on 1954 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental and Predicted Lateral directional Dynamic response Characteristics of a Large Flexible 35 Degree Swept wing Airplane at an Altitude of 35 000 Feet written by Stuart C. Brown and published by . This book was released on 1956 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: Calculated simplified transfer function coefficients based on the lateral-directional equations of motion are compared with coefficients obtained by matching transient time histories with an analog computer. Aerodynamic derivatives extracted from measured transfer function coefficients are also compared with estimated derivatives. In general, good agreement between measured and estimated values was obtained.
Download or read book Experimental and Predicted Longitudinal and Lateral Directional Response Characteristics of a Large Flexible 35 Swept Wing Airplane at an Altitude of 35 000 Feet written by Henry A. Cole and published by . This book was released on 1957 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental and Predicted Lateral directional Dynamic response Characteristics of a Large Flexible 35 degrees Swept wing Airplane at an Altitude of 35 000 Feet written by Stuart C. Brown and published by . This book was released on 1956 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Experimental and Predicted Lateral Directional Dynamic Response Characteristics of a Large Flexible 35 Deg Swept Wing Airplane at an Altitude of 35 000 Feet written by and published by . This book was released on 1956 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: The lateral-directional dynamic-response characteristics of a large flexible airplane are presented for flight conlitions of 0.6 to 0.82 Mach number and an altitude of 35,OOO feet. Transient responses at various stations on the airplane to aileron and rudder pulse-type disturbances have been recorded and converted into frequency-response form. A frequency range of O.5 to 25 radians per second is presented, which includes the Dutch roll and rolling modes and also three structural modes The measured frequency responses are compared with those obtained from transfer functions based on the lateral-directional equations of motion, which include first-order effects of structural deflections. Reasonably good agreement is obtained in the low frequency range corresponding to the lateral-directional modes. However, in the higher frequency range, the effects of the structural modes are sufficiently large so that these predictions become inadequate even for the quantities measured near the center of gravity. Comparisons are also made with frequency responses obtained from transfer-function coefficients calculated for the rigid airplane to indicate the effects of flexibility. Calculated simplified transfer function coefficients based on the lateral-directional equations of motion are compared with coefficients obtained by matching transient time histories with an analog computer. Aerodynamic derivatives extracted from measured transfer function coefficients are also compared with estimated derivatives. In general, good agreement between measured and estimated values was obtained.
Download or read book Laboratory Report LR written by National Aeronautical Establishment (Canada) and published by . This book was released on 1958 with total page 478 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Report written by and published by . This book was released on 1957 with total page 900 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Annual Report National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Note written by United States. National Aeronautics and Space Administration and published by . This book was released on 1959 with total page 744 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1954 with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Comparison of Several Methods for Estimating Low speed Stability Derivatives for Two Airplane Configurations written by Herman S. Fletcher and published by . This book was released on 1971 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Methods presented in five different publications have been used to estimate the low-speed stability derivatives of two unpowered airplane configurations. One configuration had unswept lifting surfaces, the other configuration was the D-558-II swept-wing research airplane. The results of the computations were compared with each other, with existing wind-tunnel data, and with flight-test data for the D-558-II configuration to assess the relative merits of the methods for estimating derivatives. The results of the study indicated that, in general, for low subsonic speeds, no one text appeared consistently better for estimating all derivatives.
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 770 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Aeronautical Report written by National Research Council Canada and published by . This book was released on 1960 with total page 762 pages. Available in PDF, EPUB and Kindle. Book excerpt:
