Download or read book Longitudinal Stability and Drag Characteristics at Mach Numbers from 0 75 to 1 5 of an Airplane Configuration Having a 60 Degrees Swept Wing of Aspect Ratio 2 24 as Obtained from Rocket propelled Model written by A. James Vitale and published by . This book was released on 1952 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1965 with total page 1782 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Stability and Drag Characteristics at Mach Numbers from 0 8 to 1 5 of a Free flight Model Having 3 percent thick 60 Degree Triangular Wing and Horizontal Tail Surfaces written by Rowe Chapman and published by . This book was released on 1954 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight test of a rocket-propelled model having 60 degree triangular wing and horizontal tail surfaces 3 percent thick was made to investigate the stability and drag of the configuration. Drag and stability data are compared with similar triangular-wing configurations.

Download or read book Longitudinal Stability Characteristics at Transonic Speeds of a Rocket propelled Model of an Airplane Configuration Having a 45 Degree Swept Wing of Aspect Ratio 6 0 written by John C. Jr McFall and published by . This book was released on 1954 with total page 34 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 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:

Download or read book Longitudinal Aerodynamic Characteristics of a High subsonic speed Transport Airplane Model with a Cambered 40 Sweptback Wing of Aspect Ratio 8 at Mach Numbers to 0 96 written by Atwood R. Heath and published by . This book was released on 1960 with total page 92 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Aerodynamic Characteristics at Mach Numbers from 0 50 to 1 19 of a Supersonic Transport Model with a Modified M Wing written by Edward J. Ray and published by . This book was released on 1967 with total page 84 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Lift Drag and Longitudinal Stability at Mach Numbers from 1 4 to 2 3 of a Rocket powered Model Having a 52 5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces written by Warren Jr Gillespie and published by . This book was released on 1955 with total page 29 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability and Control Characteristics at Mach Numbers of 1 41 and 2 01 of a 67 Degree Swept wing Airplane Configuration with Canard Control Surfaces written by M. Leroy Spearman and published by . This book was released on 1958 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Longitudinal Stability Characteristics at Transonic Speeds of a Canard Configuration Having a 45 Degree Sweptback Wing of Aspect Ratio 6 0 and NACA 65A009 Airfoil Section written by A. James Vitale and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flight investigation has been conducted to determine the longitudinal stability, lift, and drag characteristics at transonic speeds of a rocket-powered model of a canard configuration having a 45 degree swept-back wing of aspect ratio 6.0, taper ratio of 0.6, and NACA 65A009 airfoil section. The canard surface had an aspect ratio of 4.0 and 45 degrees of sweepback. The variations with Mach number of lift, drag, and longitudinal stability for the canard configuration are compared with a tailless and a conventional or tail-last model having the same wing.

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 Deg written by and published by . This book was released on 1960 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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.

Download or read book Longitudinal Stability Investigation for a Mach Number Range of 0 8 to 1 7 of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail written by John C. McFall and published by . This book was released on 1956 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: An airplane configuration model having a 45 degree swept wing of aspect ratio 4.0 and taper ratio of 0.3 with a low swept horizontal tail has been flown in a longitudinal stability investigation over a Mach number range of 0.8 to 1.7. Longitudinal aerodynamic coefficients and stability derivatives for the configuration are presented as functions of Mach number over the test range. Comparisons of lift-curve slopes are made with wind-tunnel data and comparisons of tail effectiveness are made with rocket-model data, and show generally good agreement. Absence of an unstable break in the pitching-moment curve, usually associated with this wing, indicates a favorable location of the horizontal tail for the lift and Mach number range of the investigation.

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:

Download or read book Longitudinal Aerodynamic Characteristics of Several High drag Bodies at Mach Numbers from 1 50 to 4 63 written by James F. Campbell and published by . This book was released on 1967 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: