Author : M. Leroy Spearman
Publisher :
Page : 36 pages
File Size : 43,9 MB
Release : 1977
Category : Aerodynamics
ISBN :
Author : M. Leroy Spearman
Publisher :
Page : 34 pages
File Size : 29,41 MB
Release : 1977
Category : Aerodynamics
ISBN :
Author : M. Leroy Spearman
Publisher :
Page : 24 pages
File Size : 45,74 MB
Release : 1977
Category : Aerodynamics
ISBN :
Author : William J. Monta
Publisher :
Page : 36 pages
File Size : 49,13 MB
Release : 1971
Category : Aerodynamics
ISBN :
Author : Organisation du traité de l'Atlantique Nord. Groupe consultatif pour la recherche et le développement aérospatial
Publisher :
Page : 758 pages
File Size : 47,14 MB
Release : 1988
Category : Guided missiles
ISBN : 9789283504528
Author :
Publisher :
Page : 670 pages
File Size : 46,87 MB
Release : 1967
Category : Aeronautics
ISBN :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author : M. Leroy Spearman
Publisher :
Page : 52 pages
File Size : 42,22 MB
Release : 1967
Category : Guided missiles
ISBN :
An investigation has been conducted in the Langley Unitary Plan wind tunnel at Mach numbers from 1.50 to 4.63 to determine the aerodynamic characteristics of a maneuverable missile having in-line cruciform wings and canard surfaces oriented in 45° roll planes.
Author : Earl D. Knechtel
Publisher :
Page : 36 pages
File Size : 47,49 MB
Release : 1956
Category : Charts, diagrams, etc
ISBN :
An experimental investigation was conducted to determine the longitudinal aerodynamic characteristics at transonic speeds of missile configurations having three blunted cone-cylinder bodies. Modifications of the basic model were tested to indicate the effects of (a) relative lengths of coplanar bodies, (b) seals between the cylindrical portions of the bodies, (c) horizontal connecting surfaces near the rear of the bodies, and (d) triangular rather than coplanar body grouping. Lift, drag, and pitching-moment data were obtained at angles of attack from -4 to 12 degrees and Mach numbers from 0.6 to 1.4 for a constant Reynolds number of 5,500,000, based on average body length.
Author : Edward J. Ray
Publisher :
Page : 88 pages
File Size : 37,72 MB
Release : 1967
Category :
ISBN :
Author : National Aeronautics and Space Administration (NASA)
Publisher : Createspace Independent Publishing Platform
Page : 30 pages
File Size : 23,19 MB
Release : 2018-07-25
Category :
ISBN : 9781724228208
Longitudinal aerodynamic characteristics of a Sparrow 3 wing control missile model were measured through a range of separation distances relative to a flat plate surface that represented the parent-body configuration. Measurements were obtained with and without two dimensional circular arc protuberances attached to the flat plate surface. The tests were conducted at a Mach number of 2.86 and a Reynolds number per meter of 6.56 million. The behavior of these longitudinal characteristics with varying separation distance in the flow field created by the flat plate and protuberance was generally as would be expected on the basis of flow field boundaries determined from the second order approximation of Friedrich. In general, varying roll angle from 0 deg to 45 deg caused no significant effect on the store separation characteristics. Stallings, R. L., Jr. Langley Research Center NASA-TM-85713, L-15705, NAS 1.15:85713 RTOP 505-43-23-02
