Download or read book Flight Measurements of the Lateral Stability and Control Characteristics of a High speed Fighter Airplane written by H. L. Crane and published by . This book was released on 1952 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Measurements of the Lateral and Directional Stability Control Characteristics of an Airplane Having a 35 Degree Sweptback Wing with 40 percent span Slots and a Comparison with Wind tunnel Data written by S. A. Sjoberg and published by . This book was released on 1948 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contains flight measurements of the low-speed lateral and directional stability and control characteristics having a 35 degree sweptback wing with 40-percent-span slots. A 1/4.5-scale mode of the airplane was tested in the Langley 300 mph 7- by 10-foot tunnel and wherever possible a comparison of flight and wind-tunnel measurements is included.

Download or read book Investigation of the Dynamic Lateral Stability and Control Characteristics of a Model of a Fighter Airplane Without a Horizontal Tail and Equipped with Either Single Or Twin Vertical Tails written by John W. Draper and published by . This book was released on 1949 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Measurements of Flying Qualities of an F 47D 30 Airplane to Determine Longitudinal Stability and Control and Stalling Characteristics written by Christopher C. Kraft and published by . This book was released on 1953 with total page 75 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight tests have been made to determine the longitudinal stability and control and stalling characteristics of an F-47D-30 airplane. The results of these tests show the airplane to be unstable with stick free in any power-on condition even at the most forward center-of-gravity postion tested. At the rearward center-of-gravity position tested the airplane also had a neutral to negative stick-fixed stability with power on. The characteristics in accelerated flight were acceptable at the forward center-of-gravity position at low and high altitudes except at high speed where the control-force variations with acceleleration were high. At the rearward center-of-gravity position, elevator-force reversals were experienced in turns at low speeds, and the elevator-force variations with acceleration were low at all the other speeds tested. Ample stall warning was afforded in all the conditions tested and the stalling characteristics were satisfactory except in the approach and wave-off conditions.

Download or read book Flight Stability and Automatic Control written by Robert C. Nelson and published by WCB/McGraw-Hill. This book was released on 1998 with total page 441 pages. Available in PDF, EPUB and Kindle. Book excerpt: The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1949 with total page 664 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 Control system Techniques for Improved Departure spin Resistance for Fighter Aircraft written by Luat T. Nguyen and published by . This book was released on 1980 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Evaluation of the Effects of Leading edge slat Span on the Stability and Control Characteristics of a Swept wing Fighter type Airplane During Accelerated Longitudinal Maneuvers at Transonic Speeds written by Gene J. Matranga and published by . This book was released on 1958 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Additional Flight Evaluations of Various Longitudinal Handling Qualities in a Variable stability Jet Fighter written by Charles R. Chalk and published by . This book was released on 1958 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Measurements of the Stability Control and Stalling Characteristics of an Airplane Having a 35 Degree Sweptback Wing Without Slots and with 80 percent span Slots and a Comparison with Wind tunnel Data written by S. A. Sjoberg and published by . This book was released on 1948 with total page 85 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report contains the results of flight measurements at low speed of the stability and control characteristics of an airplane having a 35 degree sweptback wing. The lateral and directional stability and control characteristics are presented for the airplane without slots and with 80-percent-span slots on the wing. The longitudinal stability, stalling, and lift characteristics are presented for the airplane with 80-percent-span slots.

Download or read book The Effect of Lateral Area on the Lateral Stability and Control Characteristics of an Airplane as Determined by Tests of a Model in the Langley Free flight Tunnel written by Hubert M. Drake and published by . This book was released on 1946 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The effects of large variations of lateral area on the lateral stability and control characteristics of a free-flying model when ailerons are used as the principal control have been determined by flight tests in the Langley free-flight tunnel. The effects of the lateral-force parameter (rate of change of lateral-force coefficient with angle of sideslip) were investigated for a wide range of values of the directional-stability parameter (rate of change of yawing-moment coefficient with angle of sideslip) and the rotary-damping-in-yaw parameter (rate of change of yawing-moment coefficient with yawing angular velocity).

Download or read book Flight Investigation Using Variable stability Airplanes of Minimum Stability Requirements for High speed High altitude Vehicles written by Norman M. McFadden and published by . This book was released on 1961 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Measurements of the Lateral and Directional Stability and Control Characteristics of an Airplane Having a 36 Deg Sweptback Wing With 40 Percent Span Slots and a Comparison With Wind Tunnel Data written by and published by . This book was released on 1948 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight tests have been conducted to determine the lateral and directional stability and control characteristics of an airplane on which the wing panels are swept back 35 deg. For these tests, the wings are equipped with slots extending from 40 to 80 percent of the span of the sweptback wing panels measured from the inboard end. Wind-tunnel tests were made. of a model of the airplane and wherever possible the flight and wind-tunnel data have been compared.

Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 922 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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.