By Delany, Noel K; Sorensen, Norman E
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19930083675_1993083675.pdf
PRESSURE AND FORCE CHARACTERISTICS OF NONCIRCULAR CYLINDERS AS AFFECTED BY REYNOLDS NUMBER WITH A METHOD INCLUDED FOR DETERMINING THE POTENTIAL FLOW ABOUT ARBITRARY SHAPES
by EDWARD C. POLHAMUS, EDWARD W. GELLER, and KALMAN J. GRUNWALD
TECHNICAL REPORT R-46
EFFECT OF FLOW INCIDENCE AND REYNOLDS NUMBER ON LOW-SPEED AERODYNAMIC CHARACTERISTICS OF SEVERAL NONCIRCULAR CYLINDERS WITH APPLICATIONS TO DIRECTIONAL STABILITY AND SPINNING
by Edward C. Polhamus, NACA NOTE 4176
http://naca.central.cranfield.ac.uk/reports/1958/naca-tn-4176.pdf
ou : http://naca.larc.nasa.gov/reports/1958/naca-tn-4176/
DRAG OF CYLINDERS OF SIMPLE SHAPES
By W. F. Lindsey, Report N° 619
Langley Memorial Aeronautical Laboratory, National Advisory Committee For Aeronautics October 27, 1937
A REASSESSMENT OF HEAVY-DUTY TRUCKAERODYNAMIC DESIGN FEATURES AND PRIORITIES
Edwin J. Saltzman, Robert R. Meyer, Jr. , NASA/TP-1999-206574 , June 1999
www.nasa.gov/centers/dryden/pdf/88628main_H-2283.pdf
Un texte auquel nous n’avons pas eu accès, hormis sa première page et des citations :
AERODYNAMIC CHARACTERISTICS OF CONFIGURATIONS HAVING BODIES WITH SQUARE, RECTANGULAR, AND CIRCULAR CROSS SECTIONS
Asher Sigal and Ehud Lapidot
http://www.aiaa.org/content.cfm?pageid=406&gTable=japaperimportPre97&gID=26036
EXPERIMENTAL AERODYNAMIC CHARACTERISTICS OF MISSILES WITH SQUARE CROSS SECTIONS
Zollars, G. J. and Yechout, T. R.
TECHNICAL NOTE USAFA-TN-83-8
THE DYNAMICS AND AERODYNAMICS OF SELF-SUSTAINED LARGE ANGLE
OF ATTACK BODY SPINNING OTIONS, by James E. Brunk
Final Report, Contract No. AF 49(638)-1158, Project No. 7856, Task No. 7856-01
http://www.dtic.mil/cgi-bin/GetTRDoc?AD=AD407183&Location=U2&doc=GetTRDoc.pdf
AEROBALISTIC RANGE TESTS OF MISSILE CONFIGURATIONS WITH
NON-CIRCULAR CROSS SECTIONS,
by W. Hathaway, B. Kruggel, G. Abate, G. Winchenbach and J. Krieger; sept. 2001.
MODERN DEVELOPMENTS IN FLUID DYNAMICS, Vols I and II, by Sydney Goldstein, Oxford, The Clarendon Press 1938
Nos textes pédagogiques de la page Physique de la fusée du site Go mars ! :
http://perso.numericable.fr/fbouquetbe63/gomars/physique.htm
…et spécialement :
LA THÉORIE DES CORPS ÉLANCÉS ET LES CORPS QUI N’EN RELÈVE PAS :
http://perso.numericable.fr/fbouquetbe63/gomars/corps-elances.doc
et encore :
LA PORTANCE LINÉAIRE DU FUSELAGE :
http://perso.numericable.fr/fbouquetbe63/gomars/port_lin_fuse.doc
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