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Fluid Dynamics for the Study of Transonic Flow.
This new book leads readers step-by-step through the complexities encountered as moving objects approach and cross the sound barrier. The problems of transonic flight were apparent with the very first experimental flights of scale-model rockets when the disastrous impact of shock waves and flow sepa...
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Oxford :
Oxford University Press,
1990.
|
| Colección: | Oxford engineering science series.
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| Temas: | |
| Acceso en línea: | Texto completo |
MARC
| LEADER | 00000cam a2200000Mu 4500 | ||
|---|---|---|---|
| 001 | EBOOKCENTRAL_ocn960164898 | ||
| 003 | OCoLC | ||
| 005 | 20240329122006.0 | ||
| 006 | m o d | ||
| 007 | cr |n|---||||| | ||
| 008 | 161112s1990 enk o 000 0 eng d | ||
| 040 | |a EBLCP |b eng |e pn |c EBLCP |d OCLCO |d STF |d OCLCQ |d CNNOR |d OCLCO |d HS0 |d OCLCQ |d OCLCF |d OCLCQ |d OCLCO |d OCLCQ |d OCLCO | ||
| 020 | |a 9780195362954 | ||
| 020 | |a 0195362950 | ||
| 029 | 1 | |a AU@ |b 000065431020 | |
| 035 | |a (OCoLC)960164898 | ||
| 050 | 4 | |a TL571.R366 1990 | |
| 082 | 0 | 4 | |a 629.132/304 |
| 049 | |a UAMI | ||
| 100 | 1 | |a Ramm, Heinrich J. | |
| 245 | 1 | 0 | |a Fluid Dynamics for the Study of Transonic Flow. |
| 260 | |a Oxford : |b Oxford University Press, |c 1990. | ||
| 300 | |a 1 online resource (211 pages) | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 490 | 1 | |a Oxford Engineering Science Series ; |v v. 23 | |
| 588 | 0 | |a Print version record. | |
| 505 | 0 | |a Introduction; 1. BRIEF REVIEW OF THE BASIC LAWS OF AERODYNAMICS; Problems; 2. THE THEORY OF INVISCID TRANSONIC FLOW; 2.1. One-dimensional transonic flow; 2.2. The basic three-dimensional theory; 2.2.1. An application of the basic theory; 2.3. Simplified transonic theory for small perturbations; 2.4. Transonic shock relations; 2.5. Similarity rules; 2.5.1. Similarity rules for two-dimensional subsonic and supersonic flows; 2.5.2. Similarity rule for two-dimensional transonic flow; 2.5.3. Similarity rule for axisymmetric subsonic and supersonic flows. | |
| 505 | 8 | |a 2.5.4. Similarity rule for axisymmetric transonic flow2.6. Solutions through asymptotic expansions; 2.6.1. Higher order transonic equations; 2.6.2. Asymptotic expansions; 2.7. The hodograph method; 2.7.1. Limitations of the hodograph approach; 2.7.2. The basic hodograph equations; 2.7.3. Some important applications of the hodograph method; 2.7.4. The transonic shock polar curves; Problems; 3. NONSTEADY TRANSONIC FLOW; 3.1. General observations; 3.2. Nonsteady transonic theory; 3.3. The pressure coefficient from nonsteady theory; Problems; 4. LIFT SLOPE AND DRAG RISE AT SONIC SPEED. | |
| 505 | 8 | |a 5. ANALYTICAL SOLUTIONS OF THE TRANSONIC CONTINUITY EQUATION5.1. Solutions of transonic equations by linearization; 5.1.1. Solutions through local linearization; 5.2. The equivalence rule; 5.2.1. The relative magnitudes of ∂u/∂x and ∂v/∂y (+∂w/∂z) in slender-body flow; 5.2.2. Basic considerations leading to the equivalence rule; 5.2.3. The formulation of the equivalence rule by Oswatitsch and Keune; 5.2.4. Comparison of the equivalence rule with the parabolic method of flow computations; 5.2.5. The area rule as the logical extension of the equivalence rule | |
| 505 | 8 | |a 5.3. Transonic flow with heat addition5.3.1. The equation for inviscid flow with heat addition; 5.3.2. The effect of heat addition on aircraft performance; Problems; 6. VISCOUS TRANSONIC FLOW; 6.1. Introduction; 6.2. The specific problems of transonic flow caused by viscous effects; 6.2.1. Shock wave-boundary layer interaction; 6.2.2. The shape of the transonic shock wave; 6.2.3. The longitudinal (compressive) viscosity; 6.3. The differential equations of viscous transonic flow; 6.3.1. Formulation of the longitudinal viscosity; 6.3.2. The small-perturbation equation of viscous transonic flow. | |
| 505 | 8 | |a 6.4. Applications of the viscous transonic equation6.4.1. Similarity solutions of partial differential equations; 6.4.2. Viscous flow through a Laval nozzle; 6.4.3. Viscous radial and spiral flow; Problems; 7. NUMERICAL METHODS OF TRANSONIC FLOW COMPUTATION; 7.1. Introduction; 7.2. The relaxation method; 7.3. The time-dependent method; 7.4. Artificial viscosity; 7.5. Convergence and concluding remarks; Problems; 8. STEPS TOWARD THE OPTIMUM TRANSONIC AIRCRAFT; 8.1. The basic problems; 8.2. The supercritical airfoil. | |
| 500 | |a 8.3. The longitudinal viscosity as a possible factor in the correct description of transonic flight. | ||
| 520 | |a This new book leads readers step-by-step through the complexities encountered as moving objects approach and cross the sound barrier. The problems of transonic flight were apparent with the very first experimental flights of scale-model rockets when the disastrous impact of shock waves and flow separations caused the aircraft to spin wildly out of control. Today many of these problems have been overcome, and this book offers an introduction to the transonic theory that has made possible many of these advances. The emphasis is on the most important basic approaches to the solution of transonic. | ||
| 590 | |a ProQuest Ebook Central |b Ebook Central Academic Complete | ||
| 650 | 0 | |a Aerodynamics, Transonic. | |
| 650 | 6 | |a Aérodynamique transsonique. | |
| 650 | 7 | |a Aerodynamics, Transonic |2 fast | |
| 776 | 0 | 8 | |i Print version: |a Ramm, Heinrich J. |t Fluid Dynamics for the Study of Transonic Flow. |d Oxford : Oxford University Press, ©1990 |
| 830 | 0 | |a Oxford engineering science series. | |
| 856 | 4 | 0 | |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=4702183 |z Texto completo |
| 938 | |a ProQuest Ebook Central |b EBLB |n EBL4702183 | ||
| 994 | |a 92 |b IZTAP | ||