Download or read book Transonic and Supersonic Wind Tunnel Test of the Action Hypervelocity Test Missile Volume 2 Drag Characteristics written by William D. Washington and published by . This book was released on 1974 with total page 381 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two wind tunnel tests were conducted at AEDC and BRL to define the stability characteristics of the ACTION hypervelocity test missile. The AEDC test investigated the transonic launch-coast phase of flight while the BRL test investigated the supersonic boost-sustain phase. The basic flight configuration was tested plus configuration which consisted of changes in the nose, canards, canard position, and flared angle. Mach numbers investigated ranged from 0.3 to 4.5 over an angle of attack range of -4 to +4 degrees at 0 degrees sideslip. The test was designated BRL 955/AEDC 289. This report is presented in two volumes. Volume 2 contains drag characteristics data. (Author).

Download or read book Transonic and Supersonic Wind Tunnel Test of the Action Hypervelocity Test Missile Volume 1 Stability Characteristics written by William D. Washington and published by . This book was released on 1974 with total page 408 pages. Available in PDF, EPUB and Kindle. Book excerpt: Two wind tunnel tests were conducted at AEDC and BRL to define the stability characteristics of the ACTION hypervelocity test missile. The AEDC test investigated the transonic launch-coast phase of flight while the BRL test investigated the supersonic boost-sustain phase. The basic flight configuration was tested plus configuration which consisted of changes in the nose, canards, canard position, and flared angle. Mach numbers investigated ranged from 0.3 to 4.5 over an angle of attack range of -4 to +4 degrees at 0 degrees sideslip. The test was designated BRL 955/AEDC 289. This report is presented in two volumes. Volume 1 contains stability characteristics data. (Author).

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Government Reports Announcements written by and published by . This book was released on 1974-11 with total page 1206 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Government Reports Index written by and published by . This book was released on 1975 with total page 908 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Government Reports Annual Index written by and published by . This book was released on 1974 with total page 900 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Government Reports Announcements Index written by and published by . This book was released on 1985 with total page 1162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Transonic Wind Tunnel Tests of a Base Drag Research Missile Model written by B. F. Gorin and published by . This book was released on 1970 with total page 583 pages. Available in PDF, EPUB and Kindle. Book excerpt: Tests were conducted in order to obtain data describing the effects of various simulated rocket exhaust plumes on the model's external flow field. Data describing the flow in the nozzle exit plane and in the model boundary layer were also obtained. Model external static pressure measurements were made and Schlieren, shadowgraph and tuft photographs were taken. The tests were conducted at Mach numbers from 0.000 to 1.200 at angles of attack from -2 to +2 degrees. The report presents details of the test program, an outline of the test procedure and the results of the investigation in tabular form. (Author).

Download or read book Transonic Wind Tunnel Tests on a Missile Model with Canard Wings written by R. E. DE Kuyper and published by . This book was released on 1973 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report is Volume 2 of a three volume series. Tables of aerodynamic test data are given, including balance cavity and base pressure coefficients, axial force for aerodynamic and thrust phases, canard position, and force and moment coefficients for a series of runs.

Download or read book Force Tests of Standard Hypervelocity Ballistic Models HB 1 and HB 2 at Mach 1 5 to 10 written by J. Don Gray and published by . This book was released on 1963 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic characteristics of two standard, hypervelocity, ballistic-type models, designated HB-1 and HB-2 were investigated in the supersonic and hypersonic regimes. The tests were conducted at nominal Mach numbers of 1.5, 2, 3, 4, 5, 8, and 10 at Reynolds numbers from 0.07 to 2.55 x 10 to the 6th power, based on body diameter, and through an angle-of-attack range from -2 to 15 deg. The effects of Mach number, Reynolds number, and model attitude on the static stability and axial-force characteristics of the two configurations were investigated. The zero-lift, forebody, axial-force coefficient, CA, for both configurations was found to be sensitive to Reynolds number variations; whereas the initial normal-force curve slope, CN alpha, and center of-pressure, xcp/l, for only the flared-tail model (HB-2) were dependent upon the Reynolds number. (Author).

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 International Aerospace Abstracts written by and published by . This book was released on 1970 with total page 1064 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Correlation of Full scale Drag Predictions with Flight Measurements on the C 141A Aircraft Phase 2 Wind Tunnel Tests Analysis and Prediction Techniques Volume 2 Wind Tunnel Test and Basic Data written by and published by . This book was released on 1974 with total page 198 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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:

Download or read book Transonic Wind Tunnel Tests on a Missile Model with Canard Wings written by R. E. DE Kuyper and published by . This book was released on 1973 with total page 666 pages. Available in PDF, EPUB and Kindle. Book excerpt: Volume 3 of a three volume report tabulates aerodynamic and thrust test data on a wind tunnel model of a guided missile with canard wings. Included are tail fin force and moment coefficients.

Download or read book Correlation of Full Scale Drag Predictions with Flight Measurements on the C 141A Aircraft Phase II written by D.G. MacWilkinson and published by . This book was released on 1974 with total page 185 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Static Stability and Drag Characteristics of a Hypersonic Aircraft Design at Mach Numbers 1 5 to 5 6 written by J. T. Best (Jr.) and published by . This book was released on 1975 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt: