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Titolo:
Lift, drag and thrust at high flight Mach number
Autore:
Pike, J;
Indirizzi:
APECS Ltd, Hawkley GU33 6NS, Hants, England APECS Ltd Hawkley Hants England GU33 6NS Hawkley GU33 6NS, Hants, England
Titolo Testata:
PHILOSOPHICAL TRANSACTIONS OF THE ROYAL SOCIETY OF LONDON SERIES A-MATHEMATICAL PHYSICAL AND ENGINEERING SCIENCES
fascicolo: 1759, volume: 357, anno: 1999,
pagine: 2141 - 2149
SICI:
1364-503X(19990815)357:1759<2141:LDATAH>2.0.ZU;2-U
Fonte:
ISI
Lingua:
ENG
Keywords:
hypersonic aerodynamics; orbiter performance; hypersonic similarity parameters; interference lift; external burning; lifting re-entry;
Tipo documento:
Article
Natura:
Periodico
Settore Disciplinare:
Physical, Chemical & Earth Sciences
Citazioni:
8
Recensione:
Indirizzi per estratti:
Indirizzo: Pike, J APECS Ltd, 3 Hawkley Hurst, Hawkley GU33 6NS, Hants, England APECSLtd 3 Hawkley Hurst Hawkley Hants England GU33 6NS , England
Citazione:
J. Pike, "Lift, drag and thrust at high flight Mach number", PHI T ROY A, 357(1759), 1999, pp. 2141-2149

Abstract

To assess the aerodynamic merits of a particular configuration it is convenient if similarity parameters can be found that allow comparison with other vehicles at different Mach numbers and lift coefficients. A pair of such similarity parameters occurs naturally in the study of 'direct' and 'interference' lift. The use of these parameters assists in the optimization of lift per unit drag at supersonic speeds. The designer can, for example, use these improvements to reduce wing size and structure mass. This paper derives these similarity parameters and illustrates their use.

ASDD Area Sistemi Dipartimentali e Documentali, Università di Bologna, Catalogo delle riviste ed altri periodici
Documento generato il 04/12/20 alle ore 22:25:29