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Transonic Lateral And Longitudinal Control Characteristics Of An F 8 Airplane Model Equipped With An Oblique Wing
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Book Synopsis Transonic Lateral and Longitudinal Control Characteristics of an F-8 Airplane Model Equipped with an Oblique Wing by : R. C. Smith
Download or read book Transonic Lateral and Longitudinal Control Characteristics of an F-8 Airplane Model Equipped with an Oblique Wing written by R. C. Smith and published by . This book was released on 1976 with total page 304 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 by : John C. McFall
Download or read book Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 written by John C. McFall and published by . This book was released on 1954 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Flight Investigation of the Lateral Control Characteristics of Short Wide Ailerons and Various Spoilers with Different Amounts of Wing Dihedral by : C. S. Draper
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:
Book Synopsis Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degrees Sweptback Wing and Tail as Obtained by the Transonic-bump Method by : M. Leroy Spearman
Download or read book Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degrees Sweptback Wing and Tail as Obtained by the Transonic-bump Method written by M. Leroy Spearman and published by . This book was released on 1948 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : John W. Draper
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:
Book Synopsis Determination of Lateral Stability Characteristics from Free-flight Model Tests, with Experimental Results on the Effects of Wing Vertical Position and Dihedral at Transonic Speeds by : Clarence L. Gillis
Download or read book Determination of Lateral Stability Characteristics from Free-flight Model Tests, with Experimental Results on the Effects of Wing Vertical Position and Dihedral at Transonic Speeds written by Clarence L. Gillis and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt: A test and analysis method is presented for determining airplane lateral stability characteristics, including aerodynamic derivatives, from flight tests of scale models. The method of analysis utilizes the rotating time-vector concept and also a quasi-static approach. Data are presented at transonic speeds for three swept-wing rocket-propelled models differing only in vertical position and dihedral of the wing. The method proved to be adequate for delineating the major effects of the geometric variations on the aerodynamic lateral stability derivatives. The effects of Reynolds number on the linearity of the static stability data for an unswept wing configuration are illustrated.
Book Synopsis Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90° by : Gerald V. Foster
Download or read book Effect of Longitudinal and Lateral Controls on Winged Reentry Configuration at Mach 1.97 and Angles of Attack Up to 90° written by Gerald V. Foster and published by . This book was released on 1961 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Modal Control of an Oblique Wing Aircraft by : James D. Phillips
Download or read book Modal Control of an Oblique Wing Aircraft written by James D. Phillips and published by . This book was released on 1989 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal-control Design Approach for High-angle-of-attack Aircraft by : Aaron J. Ostroff
Download or read book Longitudinal-control Design Approach for High-angle-of-attack Aircraft written by Aaron J. Ostroff and published by . This book was released on 1993 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aeroelastic Control of Oblique-wing Aircraft by :
Download or read book Aeroelastic Control of Oblique-wing Aircraft written by and published by . This book was released on 1986 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4.2 and 2 by : Arvo A. Luoma
Download or read book Longitudinal Stability and Control Characteristics at High Subsonic Speeds of Two Models of a Transonic Research Airplane with Wings and Horizontal Tails of Aspect Ratios 4.2 and 2 written by Arvo A. Luoma and published by . This book was released on 1950 with total page 134 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation was made in the Langley 8-foot high-speed tunnel of two transonic research airplane models for Mach numbers up to approximately 0.95. The test Reynolds number at the highest speed was 1,600,000 for one model and 2,300,000 for the other model. The models were 1/16-schale and were supported in the tunnel on a sting. The wing and horizontal tail of one model were both of aspect ratio 4.2; the wing and horizontal tail of the other model were both of aspect ratio 2. The same fuselage and vertical tail were used on both models. The sweep of the 50-percent-chord line of the wings was zero degrees; the sweep of the 75-percent-chord line of the horizontal tails was zero degrees. Both wings had NACA 65-110 airfoil sections and both horizontal tails had NACA 65-008 airfoil sections. Lift drag, and pitching moment were determined by means of a strain-gage balance within the fuselage. Tare measurements were made to eliminate the interference effect of the sting.
Book Synopsis 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 by : F. J. Keeney
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:
Book Synopsis The Calculation of Lateral Stability with Free Controls by : Gotthold Mathias
Download or read book The Calculation of Lateral Stability with Free Controls written by Gotthold Mathias and published by . This book was released on 1934 with total page 584 pages. Available in PDF, EPUB and Kindle. Book excerpt: The discussion of the structural methods for obtaining lateral stability discloses the remarkable influence of the constant fuselage and wing proportions to the yawing moments. For the effectiveness of modifications in vertical tail surfaces and tail length, these quotas - little observed heretofore, in this connection - are decisive. This also applies to the amount of dihedral of the wing with regard to the roll stability of the complete wing already existing without angle of the dihedral.
Book Synopsis Effect of Simulated In-flight Thrust Reversing on Vertical-tail Loads of F-18 and F-15 Airplane Models by : E. Ann Bare
Download or read book Effect of Simulated In-flight Thrust Reversing on Vertical-tail Loads of F-18 and F-15 Airplane Models written by E. Ann Bare and published by . This book was released on 1981 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Low-speed Longitudinal Characteristics of an Airplane Configuration Including Effects of Canard and Wing Trailing-edge Flap Controls in Combination by : Bernard Spencer
Download or read book Low-speed Longitudinal Characteristics of an Airplane Configuration Including Effects of Canard and Wing Trailing-edge Flap Controls in Combination written by Bernard Spencer and published by . This book was released on 1962 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Model-following Control for an Oblique-wing Aircraft by :
Download or read book Model-following Control for an Oblique-wing Aircraft written by and published by . This book was released on 1986 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Investigation of Lateral Control Near the Stall Flight Tests with High-wing and Low-wing Monoplanes of Various Configurations by : Fred E. Weick
Download or read book Investigation of Lateral Control Near the Stall Flight Tests with High-wing and Low-wing Monoplanes of Various Configurations written by Fred E. Weick and published by . This book was released on 1956 with total page 648 pages. Available in PDF, EPUB and Kindle. Book excerpt: These results are intended to provide quantitative flight-test information which may be useful to designers in attempting to provide for adequate low-speed control and which may be correlated with analytical analyses as presented in the third and finai report in this series (Technical Note 3677).
