Author: A. R. Maddox
Publisher:
ISBN:
Category : Loads (Mechanics).
Languages : en
Pages : 46
Book Description
In-flight Measurements of Captive Loads on a Store as Compared with Wind Tunnel and Mathematical Simulations
Author: A. R. Maddox
Publisher:
ISBN:
Category : Loads (Mechanics).
Languages : en
Pages : 46
Book Description
Publisher:
ISBN:
Category : Loads (Mechanics).
Languages : en
Pages : 46
Book Description
In-Flight Measurements of Captive Loads on a Store as Compared with Wind Tunnel and Mathematical Simulations
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
A series of flight tests were made to acquire captive loads data on a store to compare with corresponding data from several wind tunnel tests with conditions matched as closely as possible as well as with the best mathematical models available. The store consisted of a Mk 83 bomb shape mounted on a triple-ejector rack (TER) on an F-4 aircraft which was instrumented complete with a standard research boom mounted on the nose. The flight conditions spanned Mach 0.6 to 0.9 in both maneuvering and steady flight. The data show good correlation between flight test and wind tunnel for moderate subsonic Mach numbers when good geometric similarity is maintained, but there is a pronounced divergence in this agreement as the Mach number is increased. Correlation between mathematical models of this problem and the flight test show the same magnitude in loads and moments, but the trends do not always agree. This is most pronounced in the pitch plane.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
A series of flight tests were made to acquire captive loads data on a store to compare with corresponding data from several wind tunnel tests with conditions matched as closely as possible as well as with the best mathematical models available. The store consisted of a Mk 83 bomb shape mounted on a triple-ejector rack (TER) on an F-4 aircraft which was instrumented complete with a standard research boom mounted on the nose. The flight conditions spanned Mach 0.6 to 0.9 in both maneuvering and steady flight. The data show good correlation between flight test and wind tunnel for moderate subsonic Mach numbers when good geometric similarity is maintained, but there is a pronounced divergence in this agreement as the Mach number is increased. Correlation between mathematical models of this problem and the flight test show the same magnitude in loads and moments, but the trends do not always agree. This is most pronounced in the pitch plane.
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 772
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 772
Book Description
Government Reports Announcements & Index
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1114
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1114
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
Tactical Missile Aerodynamics
Author: Michael J. Hemsch
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 774
Book Description
This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.
Publisher: AIAA (American Institute of Aeronautics & Astronautics)
ISBN:
Category : Science
Languages : en
Pages : 774
Book Description
This two-volume set includes discussions of the physics of the fluid mechanics phenomena associated with tactical missile flight and the full range of prediction methods required to analyze current and future missiles. It's a valuable resource for missile aerodynamicists, designers, and researchers.
Captive Trajectory System for AEDC Supersonic Wind Tunnel (A) and Hypersonic Wind Tunnels (B) and (C)
Author: T. D. Buchanan
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
Book Description
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
Book Description
NASA SP.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 592
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 592
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 586
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 586
Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).
Comparison of Wind Tunnel and Flight Test Measurements of Static Aerodynamic Loading of a Captive Store
Author: R. E. Dix
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 122
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 122
Book Description