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Flight Investigation Of The Zero Lift Drag Of Two Ram Jet Missile Configurations At Mach Numbers From 10 To 189
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Book Synopsis Flight Investigation of the Zero-lift Drag of Two Ram-jet Missile Configurations at Mach Numbers from 1.0 to 1.89 by : Clarence A. Brown
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:
Book Synopsis 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 by : Eugene D. Schult
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:
Book Synopsis 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 by : Abraham A. Gammal
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:
Book Synopsis Wind-tunnel Investigation at Mach Numbers from 1.90 to 2.86 of a Canard-controlled Missile with Ram-air-jet Spoiler Roll Control by : A. B. Blair
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:
Book Synopsis Collection of Zero-lift Drag Data on Bodies of Revolution from Free-flight Investigations by : William E. Stoney
Download or read book Collection of Zero-lift Drag Data on Bodies of Revolution from Free-flight Investigations written by William E. Stoney and published by . This book was released on 1961 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents a compilation of most of the zero-lift drag results obtained from free-flight measurements made by the Langley Pilotless Aircraft Research Division on fin-stabilized bodies of revolution. The data are arranged on standard forms, which also contain the significant geometrical factors. Supplementary data have been provided to facilitate the determination of the body pressure drags from the measurement total drags. Summary plots and discussions have been included to provide a unified and broad picture of the effects of the body geometry on zero-lift drag.
Book Synopsis Summary of Rocket-Model Tests at Zero Lift of the Northrop Mx-775b Missile Configuration from Mach Numbers of 0. 9 To 1. 8 by : Richard G. Arbic
Download or read book Summary of Rocket-Model Tests at Zero Lift of the Northrop Mx-775b Missile Configuration from Mach Numbers of 0. 9 To 1. 8 written by Richard G. Arbic and published by BiblioGov. This book was released on 2013-07 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flight tests were conducted between Mach numbers of 0.9 and 1.8 over a Reynolds number range of 9(exp 6) to 30(exp 6) to determine the zero-lift drag and some rolling-effectiveness characteristics of the Northrop MX -775B missile with small and large body. The MX-775B is a proposed long range, supersonic, ground-to-ground missile having an arrow wing with 67.5 degree leading-edge sweep, 15 deg trailing-edge sweep, and a modified NACA 0004 airfoil section. The configuration has no horizontal tail but has wing trailing-edge elevons which serve a dual purpose as elevators and ailerons. The ratio of body frontal area to wing plan-form area is 0.0127 for the small-body configuration and 0.0330 for the large-body configuration. Five 1/4-scale models were flown permitting determination of the drag coefficient for the basic small-body configuration, the incremental drag due to the large body, the incremental drag resulting from a blunt wing trailing edge, the wing-plus-interference drag, and some rolling-effectiveness data. Results indicated that the MX-775B has low supersonic zero-lift drag, the maximum zero-lift drag coefficients being respectively 0.0125 and 0.0155 at a Mach number of M = 1803 for the small- and large-body configurations. The effect of a blunt wing trailing edge, obtained by cutting off 10 percent of the wing chord, was to increase the zero-lift drag by 13 to 21 percent. Wing-plus-interference drag accounted for 78 percent of the total drag at M = 0.9 and 70 percent at M = 195 for the small-body configuration. The ailerons produced positive rolling effectiveness for the wing stiffness of the test models and the dynamic pressures of the test.
Book Synopsis Flight Measurements at Mach Numbers from 1.1 to 1.9 of the Zero-lift Drag of a Twin-engine Supersonic Ram-jet Configuration by : Abraham Leiss
Download or read book Flight Measurements at Mach Numbers from 1.1 to 1.9 of the Zero-lift Drag of a Twin-engine Supersonic Ram-jet Configuration written by Abraham Leiss and published by . This book was released on 1952 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Subject Index to Unclassified ASTIA Documents by : Defense Documentation Center (U.S.)
Download or read book Subject Index to Unclassified ASTIA Documents written by Defense Documentation Center (U.S.) and published by . This book was released on 1960 with total page 308 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : A. Warner Robins
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:
Book Synopsis Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 by : Earl D. Knechtel
Download or read book Aerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4 written by Earl D. Knechtel and published by . This book was released on 1956 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.
Book Synopsis Aerodynamic Test and Analysis of a Slender Generic Missile Configuration by : Roger S. Gates
Download or read book Aerodynamic Test and Analysis of a Slender Generic Missile Configuration written by Roger S. Gates and published by . This book was released on 1989 with total page 14 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Rocket-powered Flight Test of a Roll-stabilized Supersonic Missile Configuration by : Robert A. Gardiner
Download or read book Rocket-powered Flight Test of a Roll-stabilized Supersonic Missile Configuration written by Robert A. Gardiner and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Normal Force, Center of Pressure, and Zero-lift Drag of Several Ballistic-type Missiles at Mach Numbers of 4.05 by : Edward F. Ulmann
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.
Book Synopsis Free-flight Measurements of the Zero-lift Drag of Several Wings at Mach Numbers from 1.4 to 3.8 by : H. Herbert Jackson
Download or read book Free-flight Measurements of the Zero-lift Drag of Several Wings at Mach Numbers from 1.4 to 3.8 written by H. Herbert Jackson and published by . This book was released on 1960 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis COLLECTION OF ZERO-LIFT DRAG DATA ON BODIES OF REVOLUTION FROM FREE-FLIGHT INVESTIGATIONS by : William E. Stoney (Jr.)
Download or read book COLLECTION OF ZERO-LIFT DRAG DATA ON BODIES OF REVOLUTION FROM FREE-FLIGHT INVESTIGATIONS written by William E. Stoney (Jr.) and published by . This book was released on 1961 with total page 200 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Some New Drag Data on the NACA RM-10 Missile and a Correlation of the Existing Drag Measurements at M-1.6 and 3.0 by : Robert J. Carros
Download or read book Some New Drag Data on the NACA RM-10 Missile and a Correlation of the Existing Drag Measurements at M-1.6 and 3.0 written by Robert J. Carros and published by . This book was released on 1954 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: The total zero-lift drag of a fin-stabilized parabolic body of revolution designated the RM-10 was investigated using 1./48-scale models launched from a gun through still air at Mach numbers near 1.6 and 3.0 and corresponding Reynolds numbers of 3.0 million and 5.0 million. Results of the present test showed that the location of transition had an important effect on the drag of this configuration. It is shown that the drag measurements of this investigation and those from other facilities can be correlated when, in addition to Mach number and Reynolds number, the effects of transition location and wall-to-free-stream temperature ration of skin friction are taken into account.
Book Synopsis Investigation of the Static Longitudinal Stability Characteristics of an Air-to-surface Canard Missile Configuration in the Transonic Mach Number Range by : Gerald L. Hunt
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:
