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Research on Hypersonic Stability Problems

Research on Hypersonic Stability Problems
Author: O. Walchner
Publisher:
Total Pages: 20
Release: 1974
Genre: Aerodynamics, Hypersonic
ISBN:

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This final report summarizes the in-house research work on hypersonic stability problems, applicable to reentry dynamics. During the period 1963 to 1974 research contributions were made in the following areas: (1) Static and dynamic stability in pitch; (2) hypersonic roll damping; (3) asymmetric nose effects; (4) non linear aerodynamics; (5) stability coefficients in nonplanar motions. This in-house research effort was terminated as of 1 July 1974.


Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles

Selected Aerothermodynamic Design Problems of Hypersonic Flight Vehicles
Author: Ernst Heinrich Hirschel
Publisher: Springer Science & Business Media
Total Pages: 512
Release: 2009-11-26
Genre: Technology & Engineering
ISBN: 354089974X

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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.


Advances in Hypersonics

Advances in Hypersonics
Author: BALLMAN
Publisher: Springer Science & Business Media
Total Pages: 448
Release: 2012-12-06
Genre: Technology & Engineering
ISBN: 1461203791

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These three volumes entitled Advances in Hypersonics contain the Proceedings of the Second and Third Joint US/Europe Short Course in Hypersonics which took place in Colorado Springs and Aachen. The Second Course was organized at the US Air Force Academy, USA in January 1989 and the Third Course at Aachen, Germany in October 1990. The main idea of these Courses was to present to chemists, com puter scientists, engineers, experimentalists, mathematicians, and physicists state of the art lectures in scientific and technical dis ciplines including mathematical modeling, computational methods, and experimental measurements necessary to define the aerothermo dynamic environments for space vehicles such as the US Orbiter or the European Hermes flying at hypersonic speeds. The subjects can be grouped into the following areas: Phys ical environments, configuration requirements, propulsion systems (including airbreathing systems), experimental methods for external and internal flow, theoretical and numerical methods. Since hyper sonic flight requires highly integrated systems, the Short Courses not only aimed to give in-depth analysis of hypersonic research and technology but also tried to broaden the view of attendees to give them the ability to understand the complex problem of hypersonic flight. Most of the participants in the Short Courses prepared a docu ment based on their presentation for reproduction in the three vol umes. Some authors spent considerable time and energy going well beyond their oral presentation to provide a quality assessment of the state of the art in their area of expertise as of 1989 and 1991.


Steady Glide Dynamics and Guidance of Hypersonic Vehicle

Steady Glide Dynamics and Guidance of Hypersonic Vehicle
Author: Wanchun Chen
Publisher: Springer Nature
Total Pages: 461
Release: 2020-11-07
Genre: Technology & Engineering
ISBN: 9811589011

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This book presents the latest researches on hypersonic steady glide dynamics and guidance, including the concept of steady glide reentry trajectory and the stability of its regular perturbation solutions, trajectory damping control technique for hypersonic glide reentry, singular perturbation guidance of hypersonic glide reentry, trajectory optimization based on steady glide, linear pseudospectral generalized nominal effort miss distance guidance, analytical entry guidance and trajectory-shaping guidance with final speed and load factor constraints. They can be used to solve many new difficult problems in entry guidance. And many practical engineering cases are provided for the readers for better understanding. Researchers and students in the fields of flight vehicle design or flight dynamics, guidance and control could use the book as valuable reference.


Aerodynamic Problems of Hypersonic Vehicles

Aerodynamic Problems of Hypersonic Vehicles
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
Total Pages: 250
Release: 1972
Genre: Aerodynamics, Hypersonic
ISBN:

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Comments on Hypersonic Boundary-layer Transition

Comments on Hypersonic Boundary-layer Transition
Author: Kenneth F. Stetson
Publisher:
Total Pages: 116
Release: 1990
Genre: Aerodynamics, Hypersonic
ISBN:

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This is a survey paper on the subject of hypersonic boundary-layer transition. Part 1 discusses boundary-layer stability theory, hypersonic boundary-layer stability experiments, and a comparison between theory and experiment. Part 2 contains comments on how many configuration and flow parameters influence transition. Part 3 discusses some additional general aspects of transition. Part 4 discusses problems of predicting transition and comments on three prediction methods. Part 5 contains some general guidelines for prediction methodology. Keywords: Boundary layer transition, Boundary layer stability, Hypersonic boundary layers.


On Stability and Control of Hypersonic Vehicles

On Stability and Control of Hypersonic Vehicles
Author:
Publisher:
Total Pages:
Release: 2009
Genre: Aerodynamics, Hypersonic
ISBN:

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This report has been produced in order to address aerodynamic characteristics and stability and control issues relating to hypersonic vehicles that are deemed to be significantly different from those of the conventional (subsonic or supersonic) air vehicles. In particular we have addressed issues that are relevant to stability and control of hypersonic vehicles. This report should add to the existing knowledge of missile guidance and control engineers and make, other researchers and engineers involved in hypersonic experimentation, aware that these vehicles may not be dynamically stable and require active control augmentation in order to achieve and maintain desirable flight characteristics.