Author: Defense Dept. / Sudoc Stem: D 117.8/2 - Blacklight Search Results

Start Over Author Defense Dept. Sudoc Stem D 117.8/2

321. USAAVLABS technical report. 70-37. XV-11A flight test program ; by L. J. Mertaugh, S. C. Roberts, N. S. Klran.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Feb. 1971
SuDoc number:: D 117.8/2:(nos.)

322. USAAVLABS technical report. 71-3. Application of resonant combustor to Army aircraft engine starting, final report [with list of literature cited] ; by R. L. Blnsley.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Feb. 1971
SuDoc number:: D 117.8/2:(nos.)

323. USAAVLABS technical report. 68-75. Thermal ram, new concept for load application [with list of references]; by W. H. Horton, S. C. Bailey, Strether Smith, Jan. 1969.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: [October 1969]
SuDoc number:: D 117.8/2:(nos.)

324. USAAVLABS technical reports. 70-22. Crash survival design guide [with lists of references cited]; by J. W. Turnbow [and others].

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: Revised Aug. 1969. [1969.]
SuDoc number:: D 117.8/2:(nos.)

325. USAAVLABS technical report. 69-50. Exploratory study of nature of helicopter rotor blade boundary layers [with list of literature cited]; by H. R. Veloff [and others].

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: July 1969
SuDoc number:: D 117.8/2:69-50

326. USAAVLABS technical report. 68-90c. Single-stage axial compressor component development for small gas turbines, v. 3, Supersonic compressor stage development by Charles H. Muller, Leslie R. Cox.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: June 1969
SuDoc number:: D 117.8/2:(nos.)

327. USAAVLABS technical report. 69-17. Reliability evaluation of mechanical stability augmentation system for helicopters [with list of references]; by Mario. M. George, Eugene Kisielowski, Edmund M. Fraundorf.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: June 1969
SuDoc number:: D 117.8/2:(nos.)

328. USAAVLABS technical report. 68-49D. Investigation of dynamic stability characteristics of quad configuration. ducted propeller V/STOL model: v. 4, Longitudinal stability characteristics of quad configuration, ducted-propeller V/STOL model at high duct incidence [with list of references]; by Howard C. Curtiss, jr.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: May 1969
SuDoc number:: D 117.8/2:(nos.)

329. USAAVLABS technical report. 68-57. Installation of high-reduction-ratio transmission in UH-1 helicopter [with bibliography]; by C. W. Bowen, C. E. Braddock, R. D. Walker.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: May 1969
SuDoc number:: D 117.8/2:(nos.)

330. USAAVLABS technical reports. 69-23. Fluidic vortex valve servoactuator development; by T. S. Honda, F. S. Ralbovsky.

Corporate/Agency Authors:: Army Department and Defense Dept.
Publisher:: Army Department
Date:: May 1969
SuDoc number:: D 117.8/2:(nos.)

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