Author: Sturat L. TreonPublisher:
ISBN:
Category :
Languages : en
Pages : 26
Book Description
Lateral-directional Aerodynamic Characteristics of Several Coplanar Triple-body Missile Configurations at Mach Numbers from 0.6 to 1.4
Author: Sturat L. TreonAerodynamic Characteristics in Pitch of Several Triple-body Missile Configurations at Mach Numbers 0.6 to 1.4
Author: Earl D. KnechtelPublisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 36
Book Description
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.
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1116
Book Description
Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins
Author: William J. MontaPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Scientific and Technical Aerospace Reports
Author: Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Fixed-span Missile with Three Wing Planforms
Author: M. Leroy SpearmanPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Investigation of the Aerodynamic Characteristics of a Model of a Rocket Missile with Several Arrangements of Folding Fins at Mach Numbers of 1.75, 2.15, 2.48, and 2.87
Author: Longitudinal Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.86 for a Spanmissile with Three Wing Planforms
Author: M. Leroy SpearmanPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 34
Book Description
Effect of Nose Bluntness and Afterbody Shape on Aerodynamic Characteristics of a Monoplanar Missile Concept with Bodies of Circular and Elliptical Cross Sections at a Mach Number of 2.50
Author: Ernald B. GravesPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 100
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 2088
Book Description