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The calculation of adiabatic laminar boundary layer shock wave interactions in axi-symmetric flow

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Titel

The calculation of adiabatic laminar boundary layer shock wave interactions in axi-symmetric flow

Beschreibung

The calculation of adiabatic laminar boundary layer shock wave interactions in axi-symmetric flow

Physische Beschreibung

v. ; 29 cm.

Ort der Veröffentlichung

Rhode saint Genese

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BELGIO

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INGLESE

Quelle

Biblioteche SBN Sardegna

IT\ICCU\RMS\2309626

Ressourcenverbindungen

http://id.sbn.it/bid/RMS2309626

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A parametric study of adiabatic laminar boundary layer- shock wave interactions by the method of lees-reeves-klineberg

Autor : Riethmuller, M.L.

Jahr : 1970

An experimental and theoretical investigation of adiabatic laminar boundary layer : shock wave interactions on curved walls

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None. [Part 2]: 4. Characteristics of laminar and turbulent flow (26 min) ; 5. Form, drag, lift, and propulsion (24 min) ; 6. Effects of fluid compressibility (17 min)

Jahr : 1990

None. [Part 2]: 4. Characteristics of laminar and turbulent flow (26 min) ; 5. Form, drag, lift, and propulsion (24 min) ; 6. Effects of fluid compressibility (17 min)

Jahr : 1990

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The calculation of adiabatic laminar boundary layer shock wave interactions in axi-symmetric flow

Etikett

Master resistivity curves for a two-, three-, and four-layer earth

The construction of the missile base in Comiso can be prevented!

A parametric study of adiabatic laminar boundary layer- shock wave interactions by the method of lees-reeves-klineberg

An experimental and theoretical investigation of adiabatic laminar boundary layer : shock wave interactions on curved walls

None. [Part 2]: 4. Characteristics of laminar and turbulent flow (26 min) ; 5. Form, drag, lift, and propulsion (24 min) ; 6. Effects of fluid compressibility (17 min)

None. [Part 2]: 4. Characteristics of laminar and turbulent flow (26 min) ; 5. Form, drag, lift, and propulsion (24 min) ; 6. Effects of fluid compressibility (17 min)

Queen of the wave

The days on stage!

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