Naval Postgraduate School
Theses and Dissertations
Now showing items 1-10 of 34
The effect of component redundancy upon aircraft combat survivability.
(Monterey, California. Naval Postgraduate School, 1983-12)
Aircraft combat survivability has developed into a
discipline of its own. This thesis presents a brief overview
of the two integral parts of survivability, susceptibility
and vulnerability. It examines the probability ...
Development of the A-6E/A-6E TRAM/KA-6D NATOPS Calculator Aided Performance Planning System (NCAPPS).
(Monterey, California. Naval Postgraduate School, 1983-12)
The performance data contained in the Naval Air Training
and Operating Procedures Standardization (NATOPS) manuals
for Naval aircraft are presented primarily in graphical
form. Interpretation of these graphical charts ...
Computer programs for helicopter data display and conceptual design
(Monterey, California. Naval Postgraduate School, 1983-12)
This thesis allows a person with access to a computer
that uses th= FORTRAN language and that is equipped with the
DI5SPLA software system the ability to select and
graphically portray for analysis the critical ...
Computer program to simulate digital computer based longitudinal flight control laws in a high performance aircraft
(1983-12)
The IEH Company's Continuous Systems Modeling Program
was used to simulate the longitudinal flight control system
of the F/A-18 aircraft. The model is intended for use in
investigations cf aircraft response to flight ...
Educational aids in aircraft combat survivability
(Monterey, California. Naval Postgraduate School, 1983-12)
This thesis presents four additions prepared for the text-book "The Fundamentals of Aircraft Survivability Analysis and Design, by Professor Robert E. Ball. A set of homework problems with solutions was developed for the ...
Survivability design guidelines for Fly-By-Wire Flight Control Systems development.
(Monterey, California. Naval Postgraduate School, 1983-12)
Survivability of military combat aircraft has received increased emphasis
by the U.S. Armed Services in recent years. The primary objective of the
U.S. Military Survivability Policy is to ensure that effective survivabil ...
Experimental determination of the relative flow at the tip of a transonic axial compressor rotor
(Monterey, California. Naval Postgraduate School, 1983-09)
The goal in the present work was to examine the flow through the tip section of a transonic compressor rotor in three different ways: (1) using high response instrumentation in the compressor itself, (2) using a blow-down ...
Determination of boundary layer transition and separation on double arc compressor blades in a large subsonic cascade.
(1983-09)
The china clay technique for flow visualization was used
to determine the surface flow on a double circular arc (DCA)
compressor blade in a large rectilinear subsonic cascade wind
tunnel. A calibration experiment using ...
Computer programs for helicopter high speed flight analysis
(1983-09)
This report gives the user of HP41-CV handheld programmable calculator or the IBM 3033 calculator, a blade
element method for calculating the total power required in
forward, straight and level high speed flight for ...
Guide for conceptual helicopter design
(Monterey, California. Naval Postgraduate School, 1983-06)
A conceptual helicopter design method utilizing closed form formulas and approximations from
historical data is developed for use in a helicopter design course. The design manual is to be used for the conceptual design ...
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