Author: Eugene D. SchultPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 52
Book Description
Free-flight Investigation at Mach Numbers Between 0.5 and 1.7 of the Zero-lift Rolling Effectiveness and Drag of Various Surface, Spoiler, and Jet Controls on an 80° Delta-wing Missile
Author: Eugene D. SchultPublisher:
ISBN:
Category : Mach number
Languages : en
Pages : 52
Book Description
Index of NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 500
Book Description
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 860
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 218
Book Description
Index to NASA Technical Publications
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category :
Languages : en
Pages : 208
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 2106
Book Description
February issue includes Appendix entitled Directory of United States Government periodicals and subscription publications; September issue includes List of depository libraries; June and December issues include semiannual index.
A New Dimension, Wallops Island Flight Test Range
Author: Joseph Adams ShortalPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 808
Book Description
NASA Technical Report
Author: Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 540
Book Description
Summary of Roll Controls Applicable to Fin-stabilized Vehicles
Author: Eugene D. SchultPublisher:
ISBN:
Category : Fins (Anatomy)
Languages : en
Pages : 32
Book Description
This paper discusses the rolling effectiveness of deflected fins, flaps, spoilers, and jet devices which may be employed on fin-stabilized vehicles. The possible applications and some of the significant factors affecting the performance of each device are described. The experimental information has been published previously and was obtained chiefly from free-flight tests of fin-stabilized vehicles at Mach numbers up to approximately 2.0. Comparisons are made in some cases with existing theory, which is also relied upon to indicate trends where data are not available.
Index of NASA Technical Publications
Author: Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 494
Book Description
