Flow characteristics of various swirl-can module designs

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040 ⊔ ⊔ ‡aABC ‡cABC
049 ⊔ ⊔ ‡aUIUU
090 ⊔ ⊔ ‡aTL521.3.T4 ‡bA3 no. 3236
100 1 ⊔ ‡aMularz, Edward J.
245 1 0 ‡aFlow characteristics of various swirl-can module designs / ‡cEdward J. Mularz.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1975.
300 ⊔ ⊔ ‡aiii, 37 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNASA technical memorandum ; ‡vNASA TM X-3236
500 ⊔ ⊔ ‡aPrepared at Lewis Research Center and the U.S. Army Air Mobility R&D Laboratory.
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 15-16).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aNitrogen oxides.
650 ⊔ 0 ‡aCombustion gases.
650 ⊔ 0 ‡aAircraft exhaust emissions.
650 ⊔ 0 ‡aAircraft gas-turbines ‡xCombustion chambers.
710 2 ⊔ ‡aU.S. Army Air Mobility Research and Development Laboratory.
710 2 ⊔ ‡aLewis Research Center.
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