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Effects Of Roughness Size On The Position Of Boundary Layer Transition And On The Aerodynamics Characteristics Of A 55 Swept Delta Wing At Supersonic Speeds
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Book Synopsis Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynamic Characteristics of a 55 S̊wept Delta Wing at Supersonic Speeds by : Robert L. Stallings
Download or read book Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynamic Characteristics of a 55 S̊wept Delta Wing at Supersonic Speeds written by Robert L. Stallings and published by . This book was released on 1977 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynamic Characteristics of a 55 Deg. Swept Delta Wing at Supersonic Speeds by :
Download or read book Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynamic Characteristics of a 55 Deg. Swept Delta Wing at Supersonic Speeds written by and published by . This book was released on 1977 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynmaic Characteristics of a 55° Swept Delta Wing at Supersonic Speeds by : Robert L. Stallings
Download or read book Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynmaic Characteristics of a 55° Swept Delta Wing at Supersonic Speeds written by Robert L. Stallings and published by . This book was released on 1977 with total page 47 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynamics Characteristics of a 55 ̊swept Delta Wing at Supersonic Speeds by : Robert L. Stallings
Download or read book Effects of Roughness Size on the Position of Boundary-layer Transition and on the Aerodynamics Characteristics of a 55 ̊swept Delta Wing at Supersonic Speeds written by Robert L. Stallings and published by . This book was released on 1977 with total page 52 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Memorandum written by and published by . This book was released on 1992 with total page 340 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis An Experimental Investigation of a Mach 3.0 High-speed Civil Transport at Supersonic Speeds by : Gloria Hernandez
Download or read book An Experimental Investigation of a Mach 3.0 High-speed Civil Transport at Supersonic Speeds written by Gloria Hernandez and published by . This book was released on 1993 with total page 98 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book NASA Technical Paper written by and published by . This book was released on 1986 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 836 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5 by : Peter F. Covell
Download or read book Longitudinal and Lateral-directional Aerodynamic Characteristics of a Wing-cone Configuration at Mach Numbers from 2.5 to 4.5 written by Peter F. Covell and published by . This book was released on 1992 with total page 180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Study at Low Supersonic Speeds of a Missile Concept Having Opposing Wraparound Tails by : Jerry M. Allen
Download or read book Experimental Study at Low Supersonic Speeds of a Missile Concept Having Opposing Wraparound Tails written by Jerry M. Allen and published by . This book was released on 1994 with total page 64 pages. Available in PDF, EPUB and Kindle. Book excerpt: Abstract: A wind-tunnel investigation has been performed at low supersonic speeds (at Mach numbers of 1.60, 1.90, and 2.16) to evaluate the aerodynamic characteristics of a missile concept capable of being tube launched and controlled with a simple one-axis canard controller. This concept, which features and axisymmetric body with two planar canards and four wraparound tail fins arranged in opposing pairs, must be in rolling motion to be controllable in any radial plane with the planar canards. Thus, producing a constant rolling moment that is invariant with speed and attitude to provide the motion is desirable. Two tail-fin shaping designs, one shaved and one beveled, were evaluated for their efficiency in producing the needed rolling moments, and the results showed that the shaved fins were much more desirable for this task than the beveled fins.
Book Synopsis NASA Scientific and Technical Publications by :
Download or read book NASA Scientific and Technical Publications written by and published by . This book was released on 1987 with total page 410 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalogue, United States Public Documents by :
Download or read book Monthly Catalogue, United States Public Documents written by and published by . This book was released on 1978 with total page 2248 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of a Supersonic Cruise Airplane Configuration at Mach Numbers of 2.30, 2.96, and 3.30 by : Barrett L. Shrout
Download or read book Aerodynamic Characteristics of a Supersonic Cruise Airplane Configuration at Mach Numbers of 2.30, 2.96, and 3.30 written by Barrett L. Shrout and published by . This book was released on 1979 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Monthly Catalog of United States Government Publications by :
Download or read book Monthly Catalog of United States Government Publications written by and published by . This book was released on 1978 with total page 1320 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Parametric Fin-body and Fin-plate Database for a Series of 12 Missile Fins by : Jerry M. Allen
Download or read book Parametric Fin-body and Fin-plate Database for a Series of 12 Missile Fins written by Jerry M. Allen and published by . This book was released on 2001 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt: A cooperative experimental investigation has been performed to obtain a systematic fin-body and fin-plate database for series of 12 missile fins. These data are intended to complement and extend the information contained in the Triservice missile project and to provide a systematic set of experimental data from which fin-body interference factors can be derived. Data were obtained with the fins mounted on both an axisymmetric body and on a flat plate that was used to simulate fin-alone measurements. The experiments were conducted at Mach numbers from 0.60 to 3.95; fin deflection angles of 0°, 10° , and -10° ; and angles of attack up to 30° on the body and up to 95° on the flat plate. The data were obtained from three-component balances attached to the fins and a six-component balance located in the axisymmetric body. The data obtained in this project are documented in tabular form in this report. In addition, selected data are presented in graphical form to illustrate the effects of the test variables.
Download or read book NASA SP. written by and published by . This book was released on 1962 with total page 396 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations by : Charles E. Cockrell (Jr.)
Download or read book Aerodynamic Characteristics of Two Waverider-Derived Hypersonic Cruise Configurations written by Charles E. Cockrell (Jr.) and published by . This book was released on 1996 with total page 82 pages. Available in PDF, EPUB and Kindle. Book excerpt:
