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Book Transonic and Supersonic Wind Tunnel Test of the Action Hypervelocity Test Missile  Volume 1  Stability Characteristics

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).

Book Transonic and Supersonic Wind Tunnel Test of the Action Hypervelocity Test Missile  Volume 2  Drag Characteristics

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).

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Government Reports Announcements

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:

Book Government Reports Index

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:

Book Government Reports Announcements   Index

Download or read book Government Reports Announcements Index written by and published by . This book was released on 1993-05 with total page 1306 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Wind tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1 62 scale Model of the X 1E at Supersonic Speeds

Download or read book Wind tunnel Investigation of the Static Longitudinal and Lateral Stability of a 1 62 scale Model of the X 1E at Supersonic Speeds written by Arthur Henderson and published by . This book was released on 1956 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: An investigation to determine the static longitudinal and lateral stability characteristics of a 1/62-scale model of the X-1E has been conducted in the Langley 9-inch supersonic tunnel. Tests were made at Mach numbers of 1.62, 1.94, 2.22, 2.40, and 2.62 on the wing-body, wing-body-vertical-tail, and complete model configurations. Detailed analysis of the test results has not been made.

Book Advanced Hypersonic Test Facilities

Download or read book Advanced Hypersonic Test Facilities written by Frank K. Lu and published by AIAA. This book was released on 2002 with total page 694 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Force Tests of Standard Hypervelocity Ballistic Models HB 1 and HB 2 at Mach 1 5 to 10

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).

Book Supersonic Wind Tunnel Tests of Ring wing Configurations

Download or read book Supersonic Wind Tunnel Tests of Ring wing Configurations written by Leon H. Schindel and published by . This book was released on 1958 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by and published by . This book was released on 1979 with total page 1186 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Transonic and Supersonic Wind Tunnel Tests on Control Effectiveness on Schematic Missile Configurations with Canard Controls

Download or read book Transonic and Supersonic Wind Tunnel Tests on Control Effectiveness on Schematic Missile Configurations with Canard Controls written by Sven Erik Gudmundson and published by . This book was released on 1988 with total page 74 pages. Available in PDF, EPUB and Kindle. Book excerpt: