Author: John W. Paulson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38
Book Description
Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by
Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing /by
Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70 Degree Delta Reentrry Configuration
Author: John W. Paulson
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 40
Book Description
Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing
Author: JOHN W. PAULSON
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
A model was flown over an angle-of-attack range from 10 to 35 degrees. Longitudinal stability and control characteristics were generally satisfactory with neutral or positive static longitudinal stability. The addition of artificial pitch damping resulted in satisfactory longitudinal characteristics with large amounts of static instability. The most rearward centerof-gravity position for which sustained flights could be made either with or without pitch damper corresponded to the calculated maneuver point. The lateral stability and control characteristics were satisfactory up to about 15 degree angle of attack. The damping of the Dutch roll oscillation decreassd with increasing angle of attack; the oscillation was about neutrally stable at 20 degree angle of attack and unstable at angles of attack of about 25 degrees and above. Artificial damping in roll greatly improved the lateral characteristics and resulted in flights being made up to 35 degree angle of attack. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 1
Book Description
A model was flown over an angle-of-attack range from 10 to 35 degrees. Longitudinal stability and control characteristics were generally satisfactory with neutral or positive static longitudinal stability. The addition of artificial pitch damping resulted in satisfactory longitudinal characteristics with large amounts of static instability. The most rearward centerof-gravity position for which sustained flights could be made either with or without pitch damper corresponded to the calculated maneuver point. The lateral stability and control characteristics were satisfactory up to about 15 degree angle of attack. The damping of the Dutch roll oscillation decreassd with increasing angle of attack; the oscillation was about neutrally stable at 20 degree angle of attack and unstable at angles of attack of about 25 degrees and above. Artificial damping in roll greatly improved the lateral characteristics and resulted in flights being made up to 35 degree angle of attack. (Author).
U.S. Government Research Reports
Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78° Delta Wing
Technical Abstract Bulletin
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1766
Book Description
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1766
Book Description
Investigation of Low-subsonic Flight Characteristics of a Model of a Flat-bottom Hypersonic Boost-glide Configuration Having a 78 Delta Wing
Monthly Catalog of United States Government Publications
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
Book Description
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878
Book Description
Space Scientists and Engineers: Selected Biographical and Bibliographical Listing
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340
Book Description