Download or read book Flight Investigation to Determine Lift and Drag Characteristics of a Canard Ram jet Missile Configuration in the Mach Number Range of 0 8 to 2 0 written by Abraham A. Gammal and published by . This book was released on 1954 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Investigation of the Zero lift Drag of Two Ram jet Missile Configurations at Mach Numbers from 1 0 to 1 89 written by Clarence A. Brown and published by . This book was released on 1953 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Preliminary Investigation of the Effects of Several Seeker nose Configurations on the Longitudinal Characteristics of a Canard type Missile at a Mach Number of 1 60 written by A. Warner Robins and published by . This book was released on 1958 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Investigation of the Static Longitudinal Stability Characteristics of an Air to surface Canard Missile Configuration in the Transonic Mach Number Range written by Gerald L. Hunt and published by . This book was released on 1960 with total page 24 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 52 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 108 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Normal Force Center of Pressure and Zero lift Drag of Several Ballistic type Missiles at Mach Numbers of 4 05 written by Edward F. Ulmann and published by . This book was released on 1954 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted at Mach number 4.05 to determine the aerodynamic characteristics of several missile models having turbulent boundary layers and to compare these results with available method of predicting the aerodynamic characteristics. (The condition of the boundary layer was determined by the china-clay-lacquer boundary-layer-visualization technique.) Normal force and pitching moment were measured through an angle-of-attack range of 0 to between 4 and 8 degrees, depending upon balance limitations, and at roll angles of 0 and 45 degrees; drag was measured only at 0 degrees angle of attack.

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page 860 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Flight Investigation of a Supersonic Canard Missile Equipped with an Auxiliary Damping in pitch Control System written by Martin T. Moul and published by . This book was released on 1953 with total page 36 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 1976 with total page 984 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Selected Listing of NASA Scientific and Technical Reports for written by and published by . This book was released on 1957 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Aerodynamic Characteristics at Mach Numbers from 1 50 to 4 63 of a Maneuverable Missile with In line Cruciform Wings and Canard Surfaces written by M. Leroy Spearman and published by . This book was released on 1967 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.50 to 4.63 to determine the aerodynamic characteristics of a maneuverable missile having in-line cruciform wings and canard surfaces oriented in 45° roll planes.

Download or read book Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration with a Low aspect ratio Wing and Blunt Nose at Mach Numbers from 1 2 to 2 1 written by Clarence A. Brown and published by . This book was released on 1957 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: A full-scale rocket-powered model of a cruciform canard missile configuration with a low-aspect ratio wing and blunt nose has been flight tested by the Langley Pilotless Aircraft Research Division. Static and dynamic longitudinal stability and control derivatives of this interdigitated canard-wing missile configuration were determined by using the pulsed-control technique at low angles of attack and for a Mach number range of 1.2 to 2.1.

Download or read book Aerodynamic Characteristics at Mach Numbers from 0 60 to 1 16 of a Canard Configuration Designed for Supersonic Cruise Flight 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 Three degree of freedom Evaluation of the Longitudinal Transfer Functions of a Supersonic Canard Missile Configuration Including Changes in Forward Speed written by Ernest C. Seaberg and published by . This book was released on 1954 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A reevaluation of existing flight data obtained for a supersonic canard missile configuration of the boost-glide type has been made to determine derivatives not previously evaluated. These derivatives, together with those previously evaluated and published, have been utilized to determine some typical airframe frequency responses based on the three-degree-of-freedom longitudinal equations of motion.

Download or read book Static Stability and Drag Characteristics of the HAST Missile at Mach Numbers 2 25 3 0 and 4 0 written by J. T. Best (Jr.) and published by . This book was released on 1974 with total page 194 pages. Available in PDF, EPUB and Kindle. Book excerpt: Static-force tests were conducted at Mach number 2.25, 3, and 4 on a 0.25 -scale model of the High Altitude Supersonic Target (HAST) missile.

Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Nose Mounted Canard Configurations at Supersonic Mach Numbers 1 5 Through 4 5 written by James R Burt (Jr.) and published by . This book was released on 1976 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt: Experimental aerodynamic investigations were conducted in a supersonic 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. The model was tested at angles of attack of -5 to 13 degrees and Mach numbers of 1.5 to 4.5. Aerodynamic loads were measured separately on four canards and tail panels, and the total model. The vapor screen method was used to trace the paths of the vortices shed from the canards. Roll control effectiveness of canards, both with a planar tail and a ring tail was investigated.