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 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 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 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 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 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 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 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 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 Wind Tunnel Investigation at Low Speed of a Twisted and Cambered Wing Swept Back 63 Degrees with Vortex Generators and Fences written by James A. Weilberg and published by . This book was released on 1952 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Wind tunnel Investigation at Transonic Speeds of a Jet Control on an 80 Degree Delta wing Missile written by Thomas R. Turner and published by . This book was released on 1955 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: The results indicated that the jet control is effective throughout the angle-of-attack and Mach number range investigated. The magnitude of the effectiveness increases with increase in the momentum of the jet. For jet configurations using ram air, exit-to-inlet area ratios as high as 1.28 were increasingly effective.

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 of a Large scale 25 Deg Swept wing Jet Transport Model with an External Blowing Triple slotted Flap written by and published by . This book was released on 1973 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 Static Wind tunnel and Radio controlled Flight Test Investigation of a Remotely Piloted Vehicle Having a Delta Wing Planform written by Long P. Yip and published by . This book was released on 1990 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book From Archangel to Senior Crown written by Peter W. Merlin and published by AIAA (American Institute of Aeronautics & Astronautics). This book was released on 2008 with total page 240 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Lockheed Blackbirds hold a unique place in the development of aeronautics. In their day, the A-12, YF-12, M-21, D-21, and SR-71 variants outperformed all other jet airplanes in terms of altitude and speed. Now retired, they remain the only production aircraft capable of sustained Mach 3 cruise and operational altitudes above 80,000 feet.This is the first book to address the technical aspects of these incredible aircraft. The author describes the design evolution of the Blackbird, from the Archangel to the Senior Crown (the Air Force's SR-71.) He describes in detail the construction and materials challenges faced by Lockheed, as well as the Blackbird's performance characteristics and capabilities.A NASA historian, the author describes NASA's role in using the aircraft as a flying laboratory to collect data on materials, structures, loads, heating, aerodynamics, and performance for high-speed aircraft. The reader will benefit from the technical and programmatic lessons learned.This volume was produced in cooperation with the National Aeronautics and Space Administration.