Liquid Propellant Gun Technology - download pdf or read online

By G. Klingenberg, J. Knapton, W. Morrison, G. Wren

This article seeks to supply a entire and systematic up to date remedy of liquid propellant gun expertise. The booklet discusses early ways to gun layout, equivalent to bulk-loaded configurations and using regeneratively injected bipropellants, via very contemporary advancements within the box of large-calibre and electrothermal-chemical structures. moreover, hybrid and electrothermal propulsion platforms are lined within the textual content, as are smooth ways to electrical gun improvement similar to electrothermal gun know-how. This e-book is meant for pro engineers and scientists within the fields of gun propulsion, ballistics and combustion, and for physicists, chemists and scholars - undergraduate via postgraduates - drawn to those fields. the most target of the e-book is to explain, extensive, the result of quite a few experimental and theoretical learn from 1950 until eventually the current within the box of liquid propellant propulsion. Even this present day, many of the info touching on liquid propellant gun examine continues to be scattered between army, foreign and personal documents. One advantage of utilizing this article is that the reader can locate info, formerly to be had merely via many resources, synthesized in a single booklet.

Show description

Read or Download Liquid Propellant Gun Technology PDF

Similar aeronautics & astronautics books

Anderson's Aircraft Performance and Design PDF

Written through some of the most capable aerospace authors, this new booklet develops airplane functionality concepts from first ideas and applies then to genuine airplanes. It additionally handle a philosophy of, and strategies for airplane layout. by means of constructing and discussing those matters in one textual content, the writer captures a level of synergism now not present in different texts.

Download PDF by Jerry Scutts: Mosquito in Action

Mosquito in motion half 2 КНИГИ ;ВОЕННАЯ ИСТОРИЯ Mosquito in motion half 2 (Aircraft 139)ByJerry ScuttsPublisher:Squadron/Signal courses Inc. 1993 50PagesISBN: 0897473035PDF11 MBWith the flight trying out of the Mosquito prototype ongoing, legitimate Air Ministry skepticism over the services of the wood airplane fast melted away and by surprise, the plane used to be required for each possible operational position.

Get Aircraft Noise (Cambridge Aerospace Series) PDF

Airplane Noise strains the origins of this challenge to the advent of the jet engine into the airline fleet within the past due Fifties and describes the criminal regulations now put on the undefined. It explains the derivation of the specified noise devices and evaluation scales now used worldwide; noise publicity modeling and forecasting; the foremost resources of airplane noise and their regulate; and noise dimension and prediction, together with contours.

Advanced Composite Materials for Aerospace Engineering. by Sohel Rana, Raul Fangueiro PDF

Complicated Composite fabrics for Aerospace Engineering: Processing, homes and purposes predominately specializes in using complicated composite fabrics in aerospace engineering. It discusses either the fundamental and complicated necessities of those fabrics for numerous purposes within the aerospace region, and comprises discussions on the entire major different types of advertisement composites which are reviewed and in comparison to these of metals.

Extra info for Liquid Propellant Gun Technology

Sample text

Eq. (20) is a convenient way to couple the solution of the mixing length to the flowfield. In the wake-law region of the boundary layer, locally defined eddy diffusivity is commonly used. For example, Purchased from American Institute of Aeronautics and Astronautics 34 W. E. NICOLET AND A. BALAKRISHNAN Kendall et al. 018 u e 6^ (21 where oo r I \ " uMdy (22 2 is the incompressible displacement thickness. Moss also employs locally defined eddy viscosities in his calculations of hypervelocity entry flows.

June 4-6, 1979. , 1979. All rights reserved. *Member, Technical Council, Aerospace Systems Division. Presently, president of Thermal Sciences, Inc. tStaff Engineer, Aerospace Systems Division. 26 Purchased from American Institute of Aeronautics and Astronautics PREDICTING OFF-STAGNATION-POINT FLOWFIELDS 5T = normalized turbulent mixing length, £a*/y Le = Lewis Number p = parameter used in evaluating nonsimilar integrals P = pressure P = parameter defined by Eq. (34) Pr = Prandtl Number Prv = turbulent Prandtl Number q^a = diffusive heat flux qf = radiative heat flux r = local body radius in a meridian plane R Re = radius of curvature = Reynolds Number A s = surface parallel coordinate Sc = Schmidt Number, p/yD Sc.

The important physical events encountered during planetary entry are significantly different from those met during Earth reentry. In particular, the shock-layer radiation causes massive ablation from the w a l l , which affects the entire flowfield; the viscous/mixing region assumes the character of a free shear/mixing region instead of a boundary layer. This requires a significantly different modeling approach. Transition and turbulence also are important since they change the character of the mixing layer and, consequently, the radiation flux reaching the wall.

Download PDF sample

Rated 4.65 of 5 – based on 6 votes

About the Author

admin