Download or read book Wind tunnel Investigation of a Ram jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1 60 written by M. Leroy Spearman and published by . This book was released on 1952 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation of a Ram jet Canard Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Swept Leading Edges written by M. Leroy Spearman and published by . This book was released on 1952 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation of a Ram jet Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degrees Swept Leading Edges written by Cornelius Driver and published by . This book was released on 1956 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the static stability and control characteristics of a ram-jet canard missile at a Mach number of 2.01. The missile had wings and canard surfaces of delta plan form with 70 degree swept leading edges. Two ram-jet nacelles were mounted in the vertical plane on unswept pylons near the rear of the body. The center of gravity of the model was at -19.5 percent of the wing mean aerodynamic chord. Force characteristics of the missile configuration and various combinations of its components were determined through an incidence angle range from -2 to about 26 degrees and at various roll angles from 0 to -90 degrees. The Reynolds number of the investigation was 3,470,000 based on the wing mean aerodynamic chord.
Download or read book Wind tunnel Investigation of a Ram jet Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges Force and Moment Characteristics at Combined Angles of Pitch and Sideslip for Mach Number 2 01 written by Cornelius Driver and published by . This book was released on 1956 with total page 67 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation of a Ram jet Missile Model Having a Wing and Canard Surfaces of Delta Plan Form with 70 Degree Swept Leading Edges written by Clyde V. Hamilton and published by . This book was released on 1953 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Visual QuickStart guide written by and published by . This book was released on 1999 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Mach Numbers from 1 90 to 2 86 of a Canard controlled Missile with Ram air jet Spoiler Roll Control written by A. B. Blair and published by . This book was released on 1978 with total page 106 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at a Mach Number of 2 01 of the Aerodynamic Characteristics on Combined Pitch and Sideslip of Some Canard type Missiles Having Cruciform Wings and Canard Surfaces with 70 Degrees Delta Plan Forms written by M. Leroy Spearman and published by . This book was released on 1954 with total page 121 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large scale Low speed Wind Tunnel Tests of a Model Having a 60 Degree Delta Horizontal Canard Control Surface and Wing to Obtain Static longitudinal stability and Canard surface Hinge moment Data written by Dale L. Burrows and published by . This book was released on 1954 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Wind tunnel Investigation at Supersonic Speeds of a Remote controlled Canard Missile with a Free rolling tail Brake Torque System written by and published by . This book was released on 1985 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Wind Tunnel Investigation of the Longitudinal and Lateral Aerodynamic Characteristics of a Canard Aircraft Model written by P.E. Watts and published by . This book was released on 1956 with total page 70 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Large scale Wind tunnel Tests at Low Speed of a Delta Winged Supersonic Transport Model in the Presence of the Ground written by and published by . This book was released on 1962 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Free flight Investigation at Mach Numbers Between 0 5 and 1 7 of the Zero lift Rolling Effectiveness and Drag of Various Surface Spoiler and Jet Controls on an 80 Delta wing Missile written by Eugene D. Schult and published by . This book was released on 1960 with total page 58 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book A Wind Tunnel Investigation of the Longitudinal and Lateral Aerodynamic Characteristics of a Canard Aircraft Model written by P. E. Watts and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Transonic Wind Tunnel Tests on a Missile Model with Canard Wings Volume I written by and published by . This book was released on 1973 with total page 670 pages. Available in PDF, EPUB and Kindle. Book excerpt: Transonic wind tunnel tests were performed in an Calspan Corporation (formerly Cornell Aeronautical Laboratory) Eight-Foot Transonic Wind Tunnel on a missile model with canard wings. The tests were conducted during the end of April and the beginning of May, 1973. Two distinctly different investigations were made. The effect of canard wing positions, canard - tail angular orientation, canard size, model roll angle, and nose shape, were investigated during the Aerodynamic Test Phase. The use of canard wings for roll attitude control was also investigated during this phase. The effect of different jet plumes on the aerodynamic model loads were studied during the Thrust Effect Phase. A normal jet plume simulator was used and the effects of model tail position, planform, and orientation were investigated. The report presents details of the test program and the results in tabular form.
Download or read book A Technique for Firing Dynamically Scaled Missile Models in Wind Tunnels and for Measuring Rocket motor Sound and Pressure Fluctuations written by William J. Alford and published by . This book was released on 1960 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Several Nose mounted Canard Configurations at Transonic Mach Numbers written by James R Burt (Jr.) and published by . This book was released on 1974 with total page 778 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted at the CALSPAN Corporation's transonic wind tunnel to determine the aerodynamic characteristics of several nose-mounted canard wing configurations. Canard position, geometry, angular orientation, and model nose shape were varied systematically to determine their effects on model aerodynamics. Angle of attack was varied from -3 to 12 degrees and Mach number was varied from 0.6 to 1.25. Aerodynamic loads were measured separately for each of the four canards and tail surfaces, and the total model.
