Normal view MARC view ISBD view

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability - - Washington, D.C. National Aeronautics and Space Administration 1986 - 55 p. - NASA TP 2559 : 1986 .

ISBN:

Subjects--Topical Terms:

Axisymmetric nozzles, Nonaxisymmetric nozzles, Thrust vectoring, Internal performance

Universal Decimal Class. No.: LNASA TP 2559 : 1986

Print
Add to your cart (remove)
More searches

Search for this title in:
Other Libraries (WorldCat) Other Databases (Google Scholar) Online Stores (Bookfinder.com) Open Library (openlibrary.org)