Schlichting, Hermann 1907
Overview
Works:  133 works in 459 publications in 7 languages and 4,595 library holdings 

Genres:  Conference papers and proceedings 
Roles:  Author, Editor, Honoree, Dedicatee, Creator 
Classifications:  TL574.B6, 532.052 
Publication Timeline
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Most widely held works about
Hermann Schlichting
 Hermann Schlichting100 years : scientific colloquium celebrating the anniversary of his birthday, Braunschweig, Germany 2007 by Rolf Radespiel( )
Most widely held works by
Hermann Schlichting
Boundarylayer theory by
Hermann Schlichting(
Book
)
111 editions published between 1951 and 2017 in 5 languages and held by 2,187 WorldCat member libraries worldwide
This book presents a comprehensive overview of boundarylayer theory and its application to all areas of fluid mechanics, with emphasis on the flow past bodies (e.g. aircraft aerodynamics). It contains the latest knowledge of the subject based on a thorough review of the literature over the past 15 years
111 editions published between 1951 and 2017 in 5 languages and held by 2,187 WorldCat member libraries worldwide
This book presents a comprehensive overview of boundarylayer theory and its application to all areas of fluid mechanics, with emphasis on the flow past bodies (e.g. aircraft aerodynamics). It contains the latest knowledge of the subject based on a thorough review of the literature over the past 15 years
GrenzschichtTheorie by
Hermann Schlichting(
Book
)
65 editions published between 1813 and 2006 in 6 languages and held by 574 WorldCat member libraries worldwide
Die berarbeitung fr die 10. deutschsprachige Auflage von Hermann Schlichtings Standardwerk wurde wiederum von Klaus Gersten geleitet, der schon die umfassende Neuformulierung der 9. Auflage vorgenommen hatte. Es wurden durchgngig Aktualisierungen vorgenommen, aber auch das Kapitel 15 von Herbert Oertel jr. neu bearbeitet. Das Buch gibt einen umfassenden berblick ber den Einsatz der GrenzschichtTheorie in allen Bereichen der Strmungsmechanik. Dabei liegt der Schwerpunkt bei den Umstrmungen von Krpern (z.B. Flugzeugaerodynamik). Das Buch wird wieder den Studenten der Strmungsmechanik wie auch I
65 editions published between 1813 and 2006 in 6 languages and held by 574 WorldCat member libraries worldwide
Die berarbeitung fr die 10. deutschsprachige Auflage von Hermann Schlichtings Standardwerk wurde wiederum von Klaus Gersten geleitet, der schon die umfassende Neuformulierung der 9. Auflage vorgenommen hatte. Es wurden durchgngig Aktualisierungen vorgenommen, aber auch das Kapitel 15 von Herbert Oertel jr. neu bearbeitet. Das Buch gibt einen umfassenden berblick ber den Einsatz der GrenzschichtTheorie in allen Bereichen der Strmungsmechanik. Dabei liegt der Schwerpunkt bei den Umstrmungen von Krpern (z.B. Flugzeugaerodynamik). Das Buch wird wieder den Studenten der Strmungsmechanik wie auch I
Aerodynamics of the airplane by
Hermann Schlichting(
Book
)
43 editions published between 1959 and 2013 in 3 languages and held by 391 WorldCat member libraries worldwide
"" ... Das Standardlehrbuch des Luftfahrtaerodynamikers ... "" #Luftfahrttechnik#
43 editions published between 1959 and 2013 in 3 languages and held by 391 WorldCat member libraries worldwide
"" ... Das Standardlehrbuch des Luftfahrtaerodynamikers ... "" #Luftfahrttechnik#
Aerodynamik des Flugzeuges by
Hermann Schlichting(
Book
)
34 editions published between 1960 and 2001 in German and held by 82 WorldCat member libraries worldwide
34 editions published between 1960 and 2001 in German and held by 82 WorldCat member libraries worldwide
Ludwig Prandtl collected treatises on applied mechanics, hydro and aerodynamics by
W Tollmien(
Book
)
1 edition published in 1988 in English and held by 72 WorldCat member libraries worldwide
1 edition published in 1988 in English and held by 72 WorldCat member libraries worldwide
Ludwig Prandtl collected treatises on applied mechanics, hydro and aerodynamics by
W Tollmien(
Book
)
1 edition published in 1988 in English and held by 72 WorldCat member libraries worldwide
1 edition published in 1988 in English and held by 72 WorldCat member libraries worldwide
Aerodynamik des Flugzeuges by
Hermann Schlichting(
Book
)
in German and held by 60 WorldCat member libraries worldwide
in German and held by 60 WorldCat member libraries worldwide
Grundlagen aus der Strömungsmechanik = Aerodynamik des Tragflügels (Teil 1) by
Hermann Schlichting(
Book
)
4 editions published between 1959 and 1967 in German and held by 53 WorldCat member libraries worldwide
4 editions published between 1959 and 1967 in German and held by 53 WorldCat member libraries worldwide
Aerodynamik des Tragflügels (Teil 2), des Rumpfes, der FlügelRumpfAnordnung und der Leitwerke by
Hermann Schlichting(
Book
)
4 editions published between 1969 and 2012 in German and held by 47 WorldCat member libraries worldwide
4 editions published between 1969 and 2012 in German and held by 47 WorldCat member libraries worldwide
Bian jie ceng yuan li by Shi li xi ting(
Book
)
1 edition published in 2001 in Chinese and held by 36 WorldCat member libraries worldwide
1 edition published in 2001 in Chinese and held by 36 WorldCat member libraries worldwide
Grundlagen aus der Strömungstechnik, Aerodynamik des Tragflügels (Teil 1) by
Hermann Schlichting(
Book
)
2 editions published between 2001 and 2013 in German and held by 34 WorldCat member libraries worldwide
2 editions published between 2001 and 2013 in German and held by 34 WorldCat member libraries worldwide
Hermann Schlichting100 years : scientific colloquium celebrating the anniversary of his birthday, Braunschweig, Germany
2007 by
Rolf Radespiel(
Book
)
2 editions published in 2009 in English and held by 22 WorldCat member libraries worldwide
This volume contains the contributions to the scientific anniversary colloquium in honor of the 100th birthday of Hermann Schlichting, Braunschweig, September2007. His outstanding achievements in boundary layer theory and aircraft aerodynamics are reviewed by invited scholars. Contributions of current leading research by the institutes formerly lead by Hermann Schlichting, the Institute of Fluid Mechanics of the Technische Universität Braunschweig and the Institute of Aerodynamics and Flow Technology of German Aerospace Center, in the fields of numerical flow simulation, experimental techniques, wing aerodynamics and turbomachinery highlight the lasting impact of his work until today
2 editions published in 2009 in English and held by 22 WorldCat member libraries worldwide
This volume contains the contributions to the scientific anniversary colloquium in honor of the 100th birthday of Hermann Schlichting, Braunschweig, September2007. His outstanding achievements in boundary layer theory and aircraft aerodynamics are reviewed by invited scholars. Contributions of current leading research by the institutes formerly lead by Hermann Schlichting, the Institute of Fluid Mechanics of the Technische Universität Braunschweig and the Institute of Aerodynamics and Flow Technology of German Aerospace Center, in the fields of numerical flow simulation, experimental techniques, wing aerodynamics and turbomachinery highlight the lasting impact of his work until today
Berechnung der reibungslosen inkompressiblen Strömung für ein vorgegebenes ebenes Schaufelgitter by
Hermann Schlichting(
Book
)
5 editions published in 1955 in German and held by 22 WorldCat member libraries worldwide
5 editions published in 1955 in German and held by 22 WorldCat member libraries worldwide
Threedimensional Boundary Layer Flow by
Hermann Schlichting(
Book
)
7 editions published between 1961 and 1962 in 3 languages and held by 21 WorldCat member libraries worldwide
7 editions published between 1961 and 1962 in 3 languages and held by 21 WorldCat member libraries worldwide
Untersuchungen zur Oxidation acider Thioamide und zur Darstellung von Iminomethansulfonsäurebetainen by
Hermann Schlichting(
Book
)
3 editions published in 1976 in German and held by 21 WorldCat member libraries worldwide
3 editions published in 1976 in German and held by 21 WorldCat member libraries worldwide
Über die Diffusion binärer Gasgemische in Kapillaren und porösen Stoffen by
K Eger(
Book
)
1 edition published in 1971 in German and held by 20 WorldCat member libraries worldwide
1 edition published in 1971 in German and held by 20 WorldCat member libraries worldwide
Gesammelte Abhandlungen zur angewandten Mechanik, Hydro und Aerodynamik by
Ludwig Prandtl(
Book
)
7 editions published in 1961 in German and held by 12 WorldCat member libraries worldwide
7 editions published in 1961 in German and held by 12 WorldCat member libraries worldwide
Report on the special field "interference" to the wind tunnel committee in February 1945 by
Hermann Schlichting(
Book
)
3 editions published in 1953 in English and held by 7 WorldCat member libraries worldwide
Contains an outline of investigations dealing with interference effects on the static stability of various airplane configurations that were conducted, were being conducted, and were started at the time of this report. Results of several investigations are presented and discussed briefly. A supplement is attached showing the configurations tested and outlining the various test programs. Suggestions for future investigations are also included
3 editions published in 1953 in English and held by 7 WorldCat member libraries worldwide
Contains an outline of investigations dealing with interference effects on the static stability of various airplane configurations that were conducted, were being conducted, and were started at the time of this report. Results of several investigations are presented and discussed briefly. A supplement is attached showing the configurations tested and outlining the various test programs. Suggestions for future investigations are also included
Laminar flow about a rotating body of revolution in an axial airstream by
Hermann Schlichting(
Book
)
3 editions published in 1956 in English and held by 6 WorldCat member libraries worldwide
We have set ourselves the problem of calculating the laminar flow on a body of revolution in an axial flow which simultaneously rotates about its axis. The problem mentioned above, the flow about a rotating disk in a flow, which we solved some time ago, represents the first step in the calculation of the flow on the rotating body of revolution in a flow insofar as, in the case of a round nose, a small region about the front stagnation point of the body of revolution may be replaced by its tangential plane. In our problem regarding the rotating body of revolution in a flow, for laminar flow, one of the limiting cases is known: that of the body which is in an axial approach flow but does not rotate. The other limiting case, namely the flow in the neighborhood of a body which rotates but is not subjected to a flow is known only for the rotating circular cylinder, aside from the rotating disk. In the case of the cylinder one deals with a distribution of the circumferential velocity according to the law v = omega R(exp 2)/r where R signifies the cylinder radius, r the distance from the center, and omega the angular velocity of the rotation. The velocity distribution as it is produced here by the friction effect is therefore the same as in the neighborhood of a potential vortex. When we treat, in what follows, the general case of the rotating body of revolution in a flow according to the calculation methods of Prandtl's boundarylayer theory, we must keep in mind that this solution cannot contain the limiting case of the body of revolution which only rotates but is not subjected to a flow. However, this is no essential limitation since this case is not of particular importance for practical purposes
3 editions published in 1956 in English and held by 6 WorldCat member libraries worldwide
We have set ourselves the problem of calculating the laminar flow on a body of revolution in an axial flow which simultaneously rotates about its axis. The problem mentioned above, the flow about a rotating disk in a flow, which we solved some time ago, represents the first step in the calculation of the flow on the rotating body of revolution in a flow insofar as, in the case of a round nose, a small region about the front stagnation point of the body of revolution may be replaced by its tangential plane. In our problem regarding the rotating body of revolution in a flow, for laminar flow, one of the limiting cases is known: that of the body which is in an axial approach flow but does not rotate. The other limiting case, namely the flow in the neighborhood of a body which rotates but is not subjected to a flow is known only for the rotating circular cylinder, aside from the rotating disk. In the case of the cylinder one deals with a distribution of the circumferential velocity according to the law v = omega R(exp 2)/r where R signifies the cylinder radius, r the distance from the center, and omega the angular velocity of the rotation. The velocity distribution as it is produced here by the friction effect is therefore the same as in the neighborhood of a potential vortex. When we treat, in what follows, the general case of the rotating body of revolution in a flow according to the calculation methods of Prandtl's boundarylayer theory, we must keep in mind that this solution cannot contain the limiting case of the body of revolution which only rotates but is not subjected to a flow. However, this is no essential limitation since this case is not of particular importance for practical purposes
Amplitude distribution and energy balance of small disturbances in plate flow by
Hermann Schlichting(
Book
)
3 editions published in 1950 in English and held by 5 WorldCat member libraries worldwide
The distribution of the correlation coefficient and of the amplitude of the disturbance velocities is calculated as a function of the distance from the wall for two neutral disturbances, one at the lower and one at the upper branch of the neutral stability curve. The energy balance of the disturbance motion is also investigated and it is found that as required for neutral stability the energy of the disturbance motion that is dissipated by viscosity is equal to the energy transferred to the disturbance motion from the main flow during one cycle
3 editions published in 1950 in English and held by 5 WorldCat member libraries worldwide
The distribution of the correlation coefficient and of the amplitude of the disturbance velocities is calculated as a function of the distance from the wall for two neutral disturbances, one at the lower and one at the upper branch of the neutral stability curve. The energy balance of the disturbance motion is also investigated and it is found that as required for neutral stability the energy of the disturbance motion that is dissipated by viscosity is equal to the energy transferred to the disturbance motion from the main flow during one cycle
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Related Identities
 Gersten, K. Author
 Truckenbrodt, Erich 1917
 Rossow, CordChristian
 Brinkmann, Benjamin
 Radespiel, Rolf
 Tollmien, Walter Author Editor Creator
 Krause, Egon Other Contributor
 Goertler, Henry
 United States National Aeronautics and Space Administration
 Mayes, Katherine Translator
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Associated Subjects
Aerodynamic load Aerodynamics Aerofoils Air flow AirplanesNacelles AirplanesTail surfaces AirplanesWings Astronautics Axial flow Body of revolution Boundary layer Cascades (Fluid dynamics) Diffusion Engineering Engineering mathematics Fluid dynamics Fluid mechanics Fluids Gases Hydraulic engineering Hydrodynamics Interference (Aerodynamics) Laminar flow Mathematical physics Mathematics Mechanics, Applied Physics Plates (Engineering) Stability Stability of airplanes
Alternative Names
Hermann Schlichting Duits ingenieur (19071982)
Hermann Schlichting German engineer
Hermann Schlichting tysk ingeniør
Hermann Schlichting tysk ingenjör
Schlichting, H.
Schlichting, H. 1907
Schlichting, H. 19071982
Schlichting, H. (Hermann), 1907
Schlichting, Hermann
Schlichting Herrmann
Schlichting, Herrmann 1907
Schlichting, Herrmann 19071982
Šlihting, G.
Шлихтинг, Г 19071982
Шлихтинг, Г. (Герман), 19071982
Шлихтинг, Герман
ヘルマン・シュリヒティング
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