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Stability And Control Characteristics At A Mach Number Of 201 Of A Variable Wing Sweep Configuration With Outboard Wing Panels Swept Back 75
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Book Synopsis Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75° by : M. Leroy Spearman
Download or read book Stability and Control Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with Outboard Wing Panels Swept Back 75° written by M. Leroy Spearman and published by . This book was released on 1959 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° by : Gerald V. Foster
Download or read book Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° written by Gerald V. Foster and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75° by : Gerald V. Foster
Download or read book Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75° written by Gerald V. Foster and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :448 pages Book Rating :4.F/5 ( download)
Book Synopsis NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Download or read book NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration Scientific and Technical Information Division and published by . This book was released on 1968 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Division Publisher : ISBN 13 : Total Pages :436 pages Book Rating :4.E/5 ( download)
Book Synopsis A Selected Listing of NASA Scientific and Technical Reports by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Download or read book A Selected Listing of NASA Scientific and Technical Reports written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Division and published by . This book was released on 1968 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings by : Bernard Spencer
Download or read book Stability and Control Characteristics at Low Subsonic Speeds of an Airplane Configuration Having Two Types of Variable-sweep Wings written by Bernard Spencer and published by . This book was released on 1960 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design by : Odell A. Morris
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design written by Odell A. Morris and published by . This book was released on 1961 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1966 with total page 1492 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75° by : Gerald V. Foster
Download or read book Effects of Spoiler-slot-deflector Control on the Aerodynamic Characteristics at a Mach Number of 2.01 of a Variable-wing-sweep Configuration with the Outer Wing Panels Swept Back 75° written by Gerald V. Foster and published by . This book was released on 1960 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA SP. written by and published by . This book was released on 1962 with total page 436 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Investigation of the Aerodynamic Characteristics of a Variable-sweep Supersonic Transport Configuration Having a Blended Wing and Body by : William C. Sleeman
Download or read book Low-speed Investigation of the Aerodynamic Characteristics of a Variable-sweep Supersonic Transport Configuration Having a Blended Wing and Body written by William C. Sleeman and published by . This book was released on 1961 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels by : M. Leroy Spearman
Download or read book Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.01 of a Tailless Delta V/STOL Configuration Having Variable-sweep Wing Panels written by M. Leroy Spearman and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Transonic Investigation of Aerodynamic Characteristics of a Swept-wing Fighter-airplane Model with Leading-edge Droop in Combination with Outboard Chord-extensions and Notches by : Charles F. Whitcomb
Download or read book Transonic Investigation of Aerodynamic Characteristics of a Swept-wing Fighter-airplane Model with Leading-edge Droop in Combination with Outboard Chord-extensions and Notches written by Charles F. Whitcomb and published by . This book was released on 1956 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation of the effects of several wing leading-edge modifications on the aerodynamic characteristics of a 45 degree swept-wing fighter-airplane model has been conducted in the Langley 16-foot transonic tunnel at low and high lifting conditions at Mach numbers from 0.85 to 1.03. The investigation included the determination of the effect on longitudinal stability and performance characteristics of wing leading-edge and chord-extension droops of 6 and 20 degrees, chord-extension overhangs of 0.075c and 0.15c (where c is the wing chord), leading-edge notches cut out at the inboard end of the 0.075c chord-extension to depths of 0.075c and 0.125c, and indentation of the model fuselage to conform partially to the supersonic area rule for a Mach number of 1.20. Lift, drag, and pitching-moment data were obtained for configurations with the tail on and off. Comparisons of data obtained from the present model with data from a configuration with leading-edge slats are included.
Book Synopsis Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Tactical-fighter Model with Wing Sweeps of 25, 65, 85, and 160 Degrees by :
Download or read book Transonic Longitudinal Aerodynamic Characteristics of a Variable-sweep Tactical-fighter Model with Wing Sweeps of 25, 65, 85, and 160 Degrees written by and published by . This book was released on 1962 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Wing-tip Droop on the Longitudinal Characteristics of Two Highly Swept Wing-body Combinations at Mach Numbers from 0.6 to 1.4 by : Earl D. Knechtel
Download or read book Effects of Wing-tip Droop on the Longitudinal Characteristics of Two Highly Swept Wing-body Combinations at Mach Numbers from 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1957 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stability characteristics of a 53 and a 63 degree sweptback wing-body combination. Both models were tested with flat and abruptly drooped wing tips. The 63 degree wing was also tested with a curved drooped tip. In addition, the combined effects of wing fences and extended leading-edge flaps were investigated. The results showed that abrupt droop of the outer 40 percent of the basic 53 degree wing improved the stability characteristics of the model. For the 63 degree swept wing, curved droop caused slight beneficial effects on the stability, whereas abrupt droop caused adverse effects. In general, the most favorable stability characteristics were obtained for either flat or abruptly drooped wings with fences and extended leading-edge flaps.
