High speed interference heating loads and pressure distributions resulting from elevon deflections

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High speed interference heating loads and pressure distributions resulting from elevon deflections

High speed interference heating loads and pressure distributions resulting from elevon deflections

Johnson, C.B. / Kaufman, L.G.

Effects of elevon-induced three-dimensional shock-wave turbulent boundary-layer interactions on hypersonic aircraft surfaces are analyzed. Detailed surface pressure and heating rate distributions obtained on wing-elevon fuselage models representative of aft portions of hypersonic aircraft are compared with analytical and experimental results from other sources. Examples are presented that may be used to evaluate the adequacy of current theoretical methods for estimating the effects of three-dimensional shock-wave turbulent boundary-layer interactions on hypersonic aircraft surfaces. (Kursetz)

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Title :

High speed interference heating loads and pressure distributions resulting from elevon deflections

Additional title:

Verteilung von hohen Interferenzaufheizungen und Druecken bei hohen Geschwindigkeiten als resultierende Groesse der Ausbiegung des Hoehenquerruders

Contributors:

Johnson, C.B. (author) / Kaufman, L.G. (author)

Published in:

AIAA-Papers ; Jan ; 1-7

Publication date :

1979

Size :

7 Seiten, 17 Bilder, 12 Quellen

Type of media :

Conference paper

Type of material :

Print

Language :

English

Keywords :

FLUGZEUGBAU , FLUGZEUGROLLSTEUERUNG , MACH-ZAHL , REYNOLDS-ZAHL , STROEMUNGSPROFIL , AUSLENKUNG , GRENZSCHICHTSTROEMUNG , DREIDIMENSIONALE STROEMUNG , STOSSWELLE , DRUCKVERTEILUNG , TEMPERATURVERTEILUNG , MATHEMATISCHES VERFAHREN , MODELLSIMULATION

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