Theses and Dissertations
Now showing items 1-10 of 16
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 ...
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 ...
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 ...
A microcomputer program package of the USAF stability and control DATCOM.
(Monterey, California. Naval Postgraduate School, 1983-06)
A microcomputer application program package utilizing
the methodology of the USAF STABILITY AND CONTROL DATCOM has
been implemented to estimate aircraft stability and control
derivatives. The program package is designed ...
Report of tests of a compressor configuration of DCA blading.
(Monterey, California. Naval Postgraduate School, 1983-06)
Results of an experimental program to measure the performance
of a compressor stator cascade consisting of 20
DCA blades of chord 5.01 inches, aspect ratio 2.0 and solidity
1.67 under conditions of varying incidence ...
Powerplant selection for conceptual helicopter design
(Monterey, California. Naval Postgraduate School, 1983-06)
A method of optimizing the selection of a powerplant
based upon engine and fuel weight is developed for use in
a conceptual helicopter design course. Historical data is
analyzed to verify and modify existing formulae ...
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