2 edition of Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude found in the catalog.
Thrust performance of a variable-geometry, nonaxisymmetric, two-dimensional, convergent-divergent exhaust nozzle on a turbojet engine at altitude
David M Straight
1983 by National Aeronautics and Space Administration Scieentific and Technical Information Branch, For sale by the National Technical Information Service] in Washington D.C, [Springfield, Va .
Written in English
|Statement||David M. Straight and Richard R. Cullom|
|Series||NASA technical paper -- 2171|
|Contributions||Cullom, Richard R, Lewis Research Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch|
|The Physical Object|
|Pagination||36 p. :|
|Number of Pages||36|
Desktop publishing with Microsoft Word 5.0
20 years in a Montana missile silo
Dw-1 or Where Does Breakfa
Dora Bells village cats
Anesthesia and analgesia for farm animals
Analogies of organized beings.
Horry and the Waccamaw
Development of a system to test for the toxicity of solar irradiated polynuclear aromatic hydrocarbons and preliminary data using mammalian cell cultures
Drafting letters of intent
Assignment to Berlin.
New-York, October 30, 1776. To the Kings Most Excellent Majesty.
fight for freedom
Amending the Indian Self-Determination and Education Assistance Act to provide further self-governance by Indian tribes
The research and experimentation tax credit
Have your say in May