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 PDF 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 PDF Author: John W. Paulson
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

Book Description


Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70 Degree Delta Reentrry Configuration

Investigation of the Low-subsonic Stability and Control Characteristics of a Free-flying Model of a Thick 70 Degree Delta Reentrry Configuration PDF Author: John W. Paulson
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

Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78 Degree Delta Wing PDF 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).

U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1216

Book Description


Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78° Delta Wing

Investigation of Low-subsonic Flight Characteristics of a Model of a Hypersonic Boost-glide Configuration Having a 78° Delta Wing PDF Author: John W. Paulson
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

Book Description


Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
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

Investigation of Low-subsonic Flight Characteristics of a Model of a Flat-bottom Hypersonic Boost-glide Configuration Having a 78 Delta Wing PDF Author: John W. Paulson
Publisher:
ISBN:
Category :
Languages : en
Pages : 31

Book Description


Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1878

Book Description


Space Scientists and Engineers: Selected Biographical and Bibliographical Listing

Space Scientists and Engineers: Selected Biographical and Bibliographical Listing PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 340

Book Description