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Book Aerodynamic Characteristics of Two Waverider Derived Hypersonic Cruise Configurations

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:

Book Aerodynamic Characteristics of Two Waverider Derived Hypersonic Cruise Configurations

Download or read book Aerodynamic Characteristics of Two Waverider Derived Hypersonic Cruise Configurations written by National Aeronautics and Space Adm Nasa and published by . This book was released on 2018-11-02 with total page 80 pages. Available in PDF, EPUB and Kindle. Book excerpt: An evaluation was made on the effects of integrating the required aircraft components with hypersonic high-lift configurations known as waveriders to create hypersonic cruise vehicles. Previous studies suggest that waveriders offer advantages in aerodynamic performance and propulsion/airframe integration (PAI) characteristics over conventional non-waverider hypersonic shapes. A wind-tunnel model was developed that integrates vehicle components, including canopies, engine components, and control surfaces, with two pure waverider shapes, both conical-flow-derived waveriders for a design Mach number of 4.0. Experimental data and limited computational fluid dynamics (CFD) solutions were obtained over a Mach number range of 1.6 to 4.63. The experimental data show the component build-up effects and the aerodynamic characteristics of the fully integrated configurations, including control surface effectiveness. The aerodynamic performance of the fully integrated configurations is not comparable to that of the pure waverider shapes, but is comparable to previously tested hypersonic models. Both configurations exhibit good lateral-directional stability characteristics. Cockrell, Charles E., Jr. and Huebner, Lawrence D. and Finley, Dennis B. Unspecified Center...

Book Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles

Download or read book Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles written by Ernst Heinrich Hirschel and published by Springer Science & Business Media. This book was released on 2009-11-26 with total page 512 pages. Available in PDF, EPUB and Kindle. Book excerpt: In this book selected aerothermodynamic design problems in hypersonic vehicles are treated. Where applicable, it emphasizes the fact that outer surfaces of hypersonic vehicles primarily are radiation-cooled, an interdisciplinary topic with many implications.

Book Aerodynamic Characteristics Of Two Waverider Derived Hypersonic    NASA TP 3559    Mar  7  1997

Download or read book Aerodynamic Characteristics Of Two Waverider Derived Hypersonic NASA TP 3559 Mar 7 1997 written by United States. National Aeronautics and Space Administration and published by . This book was released on 1998* with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack

Download or read book An Experimental Investigation of the Aerodynamic Characteristics of Slender Hypersonic Vehicles at High Angles of Attack written by Robert H. Feldhuhn and published by . This book was released on 1968 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt: Pressure, heat transfer, force, flow field surveys and flow visualization measurements on an inclined cone were obtained in a wind tunnel at a nominal Mach number of 6. Force measurements were also obtained for a 2/3 power law body and two ducted-cone configurations.

Book NASA Technical Memorandum

Download or read book NASA Technical Memorandum written by and published by . This book was released on 1996 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Hypersonic and High Temperature Gas Dynamics

Download or read book Hypersonic and High Temperature Gas Dynamics written by John David Anderson and published by AIAA. This book was released on 1989 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.

Book Supersonic Aerodynamics of a Class of Cone Derived Waveriders

Download or read book Supersonic Aerodynamics of a Class of Cone Derived Waveriders written by Maurice L. Rasmussen and published by . This book was released on 1981 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt: The aerodynamic properties of a new class of missile airframes that are derived from the known supersonic flow fields past inclined circular and elliptic cones are discussed. The theoretical foundations and initial force and moment data have been presented recently elsewhere. The present paper advances this knowledge in several ways. Force and moment data for two waverider configurations are presented for Mach = 8, extending the previous data taken in the range Mach = 3 to 5. Surface pressure data are also presented, and plans for future free-flight ballistic tests are discussed. The implications of the data and the underlying theory toward the design of highly maneuverable missiles with high lift and low drag, together with proposals for integrated vertical fins and blended inlets, are considered. (Author).

Book Aerodynamic Analysis of Hypersonic Waverider Aircraft

Download or read book Aerodynamic Analysis of Hypersonic Waverider Aircraft written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-07-17 with total page 104 pages. Available in PDF, EPUB and Kindle. Book excerpt: The purpose of this study is to validate two existing codes used by the Systems Analysis Branch at NASA ARC, and to modify the codes so they can be used to generate and analyze waverider aircraft at on-design and off-design conditions. To generate waverider configurations and perform the on-design analysis, the appropriately named Waverider code is used. The Waverider code is based on the Taylor-Maccoll equations. Validation is accomplished via a comparison with previously published results. The Waverider code is modified to incorporate a fairing to close off the base area of the waverider configuration. This creates a more realistic waverider. The Hypersonic Aircraft Vehicle Optimization Code (HAVOC) is used to perform the off-design analysis of waverider configurations generated by the Waverider code. Various approximate analysis methods are used by HAVOC to predict the aerodynamic characteristics, which are validated via a comparison with experimental results from a hypersonic test model. Sandlin, Doral R. and Pessin, David N. Unspecified Center AERODYNAMIC CHARACTERISTICS; APPLICATIONS PROGRAMS (COMPUTERS); DESIGN ANALYSIS; FAIRINGS; HYPERSONIC AIRCRAFT; WAVERIDERS; APPROXIMATION; COMPUTATIONAL FLUID DYNAMICS; HYPERSONICS; SYSTEMS ANALYSIS...

Book Experimental and Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts at Mach Numbers of 2 96  3 96  and 4 63

Download or read book Experimental and Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts at Mach Numbers of 2 96 3 96 and 4 63 written by and published by . This book was released on 1980 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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 1994 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental and Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts at Mach Numbers of 2 96  3 96  and 4 63

Download or read book Experimental and Theoretical Aerodynamic Characteristics of Two Hypersonic Cruise Aircraft Concepts at Mach Numbers of 2 96 3 96 and 4 63 written by Jimmy L. Pittman and published by . This book was released on 1980 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book International Aerospace Abstracts

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1996 with total page 948 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Flow field and Drag Characteristics of Several Boundary layer Tripping Elements in Hypersonic Flow

Download or read book Flow field and Drag Characteristics of Several Boundary layer Tripping Elements in Hypersonic Flow written by Allen H. Whitehead (Jr.) and published by . This book was released on 1969 with total page 44 pages. Available in PDF, EPUB and Kindle. Book excerpt: Flow field and drag characteristics of several laminar boundary layer tripping element in hypersonic flow.

Book Transonic Aerodynamic Characteristics of Two Hypersonic Cruise Configurations

Download or read book Transonic Aerodynamic Characteristics of Two Hypersonic Cruise Configurations written by Richard A. Langhans and published by . This book was released on 1969 with total page 112 pages. Available in PDF, EPUB and Kindle. Book excerpt: