Aerodynamic Characteristics of Missile Configurations with Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01.

Finding items...

Restrictions on Access: Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary: An investigation has been made in the Langley 4-by-4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a series of missile configurations having low-aspect-ratio wings at a Mach number of 2.01. The effects of wing plan form and size, length-diameter ratio, forebody and afterbody length, boattailed and flared afterbodies, and component force and moment data are presented for combined angles of attack and sideslip to about 28 degrees. No analysis of the data was made in this report.
Collection: NASA Technical Reports Server (NTRS) Collection.
Note: Document ID: 19930089792.
Accession ID: 93R19082.
NACA-RM-L57D19.
Terms of Use and Reproduction: No Copyright.

View MARC record | catkey: 15428915

Actions for Aerodynamic Characteristics of Missile Configurations with Wings of Low Aspect Ratio for Various Combinations of Forebodies, Afterbodies, and Nose Shapes for Combined Angles of Attack and Sideslip at a Mach Number of 2.01.