Download or read book Flight Investigation of the Aileron Characteristics of the Douglas D 558 I Airplane BuAero No 37972 at Mach Numbers 0 6 to 0 89 written by Jim Rogers Thompson and published by . This book was released on 1950 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Investigation of the Aileron Characteristics of the Douglas D 558 I Airplane BuAero No 37972 at Mach Numbers Between 0 6 and 0 89 written by Jim Rogers Thompson and published by . This book was released on 1950 with total page 23 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abrupt, rudder-fixed aileron rolls have been made with the Douglas D-558-1 airplane (BuAero No. 37973) at Mach numbers between 0.6 and 0.89. Rolls were made at aileron deflections between one-eighth and one-half the maximum available deflection. The results obtained indicate that the aileron effectiveness is independent of Mach number and deflection within the range investigated.

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 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 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 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Investigation of an Aileron and a Spoiler on a Wing of the X 3 Airplane Plan Form at Mach Numbers from 0 5 to 1 6 written by Roland D. English and published by . This book was released on 1954 with total page 20 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 John P. Mayer and published by . This book was released on 1950 with total page 35 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight and Wind tunnel Investigation to Determine the Aileron vibration Characteristics of 1 4 scale Wing Panels of the Douglas D 558 2 Research Airplane written by Ellwyn E. Angle and published by . This book was released on 1948 with total page 27 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 John P. Mayer and published by . This book was released on 1951 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Lift and Drag Characteristics of the Douglas D 558 II Research Airplane Obtained in Exploratory Flights to a Mach Number of 2 0 written by Jack Nugent and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Measured Characteristics of the Douglas D 558 1 Airplane BUAERO NO 37971 in Two Landings written by Hubert M. Drake and published by . This book was released on 1949 with total page 8 pages. Available in PDF, EPUB and Kindle. Book excerpt: Records were obtained of two landings of the Douglas D-558-1 airplane during the stability and control investigation. These two records show that the maximum normal-force coefficient used during the landings, 0.95, was considerably below the maximum, 1.2, estimated to be available. The approaches were made at 150 percent of the possible minimum speed, and the actual contacts were at about 115 percent of minimum speed. The rate of descent in the approach was 1200 to 1800 feet per minute at the start of the landing flare.

Download or read book Flight Measurements with the Douglas D 558 II BuAero No 37974 Research Airplane written by W.H. Stillwell and published by . This book was released on 1950 with total page 43 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 Determination of the Aerodynamic Center and Zero lift Pitching moment Coefficient of the Wing fuselage Combination by Means of Tail load Measurements in the Mach Number Range from 0 37 to 0 87 written by John P. Mayer 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 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 Longitudinal Frequency response Characteristics of the Douglas D 558 I Airplane as Determined from Experimental Transient response Histories to a Mach Number of 0 90 written by Ellwyn E. Angle and published by . This book was released on 1952 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Flight Investigation of the Lateral Control Characteristics of Short Wide Ailerons and Various Spoilers with Different Amounts of Wing Dihedral written by C. S. Draper and published by . This book was released on 1934 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2 0 written by Robert S. Osborne and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt: