Download or read book Static Longitudinal Stability and Control Characteristics of a 1 16 Scale Model of the Douglas D 558 II Research Airplane at Mach Numbers of 1 61 and 2 01 written by M. Leroy Spearman and published by . This book was released on 1953 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Lateral Stability Characteristics of a 1 16 scale Model of the Douglas D 558 II Research Airplane at Mach Numbers of 1 61 and 2 01 written by Frederick C. Grant and published by . This book was released on 1953 with total page 39 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 A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1957 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Investigation of the Longitudinal Stability and Control Characteristics of the Douglas D 558 I Airplane BuAero No 37972 at Mach Numbers Up to 0 89 written by Melvin Sadoff and published by . This book was released on 1951 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt: Results and analysis pertaining to the longitudinal stability and control characteristics of the Douglas D558-1 airplane (BuAero No. 37972) are presented. The results were obtained during shallow dives and wind-up turns at altitudes between 37,000 and 27,000 feet and at Mach numbers between 0.6 and 0.89.

Download or read book Introduction to Aircraft Flight Mechanics written by Thomas R. Yechout and published by AIAA. This book was released on 2003 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.

Download or read book Longitudinal Static Stability and Inlet Drag Characteristics of the McDonnell Douglas F 15 Tactical Fighter Aircraft at Mach Numbers of 1 60 and 2 20 written by F. J. Keeney and published by . This book was released on 1971 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Frequency response and Stability Characteristics of the Douglas D 558 II Airplane as Determined from Transient Response to a Mach Number of 0 96 written by Euclid C. Holleman and published by . This book was released on 1952 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Measurements with the Douglas D 558 II BuAero No 37974 Research Airplane written by S. A. Sjoberg and published by . This book was released on 1950 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Flight Measurements of the Static Longitudinal Stability and Stalling Characteristics of the Douglas D 558 II Research Airplane BUAERO NO 37974 written by S.A. Sjoberg and published by . This book was released on 1949 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Static Stability Characteristics of Several Preliminary Models of the X 15 Research Airplane at Mach Numbers of 2 98 and 4 01 written by Robert W. Dunning and published by . This book was released on 1959 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability Characteristics in Accelerated Maneuvers at Subsonic and Transonic Speeds of the Douglas D 558 II Research Airplane Equipped with a Leading edge Wing Chord extension written by Jack Fischel and published by . This book was released on 1954 with total page 62 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics of a Two place All weather Fighter Airplane Between Mach Numbers of 0 80 and 2 00 Obtained from the Flight Test of a Rocket boosted Model written by and published by . This book was released on 1959 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Longitudinal Directional and Lateral Stability and Control Data at a Mach Number of 6 83 of the Final Configuration of the X 15 Research Airplane written by Jim A. Penland and published by . This book was released on 1960 with total page 150 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Measurements with the Douglas D 558 II BuAero No 37974 Research Airplane written by J.V. Wilmerding and published by . This book was released on 1950 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Longitudinal Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0 80 Chord Line Unswept and with Several Tail Configurations written by Kenneth W. Goodson and published by . This book was released on 1961 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The basic aspect-ratio-4.00 wing had a zero taper and an unswept 0.80 chord line. Several aspect-ratio modifications to the basic wing were made by clipping off portions of the wing tips. The complete model was tested with a chord-plane tail, a T-tail, and a biplane tail (combined T-tail and chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92. The data show that, when reduced to the same static margin, all the tail configurations tested on the model provided fairly good stability characteristics, the biplane tail giving the best overall characteristics as regards pitching-moment linearity. Changes in static margin at zero lift coefficient with Mach number were small for the model with these tails over the Mach number range investigated.

Download or read book Compressibility Effects on the Longitudinal Stability and Control of a Pursuit type Airplane as Measured in Flight written by William N. Turner and published by . This book was released on 1945 with total page 72 pages. Available in PDF, EPUB and Kindle. Book excerpt: Measurements of the longitudinal stability and control of a pursuit-type airplane (the P-39N-1 airplane) were made in flight up to a Mach number of 0.78. The data are presented in the form of curves showing the variation, with center-of-gravity position, dynamic pressure, and Mach number, of the stick-fixed and stick-free stability, control, and balance of the airplane.