Publish Year Decade: 1950 - 1959 / Catalog Issue Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Publish Year Decade 1950 - 1959 Catalog Issue Year Decade 1960 - 1969

321. NACA research memorandum RM (series). A58A08. Experimental lift-drag ratios for 2 families of wing-body combinations at supersonic speeds [with list of references]; by Leland H. Jorgensen.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 10, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

322. NACA research memorandum RM (series). L58A20. Longitudinal and lateral stability and control characteristics at Mach no. 2.01 of 60° delta-wing airplane configuration equipped with canard control and with wing tralling-edge flap controls [with list of references]; by M. Leroy Spearman and Cornelius Driver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 10, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

323. NACA research memorandum RM (series). H58A03a. Flight evaluation of effects of leading-edge-slat span on stability and control characteristics of swept-wing tighter-type airplane during accelerated longitudinal maneuvers at transonic speeds [with list of references]; by Gene J. Matranga and Katherine H. Armistead.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

324. NACA research memorandum RM (series). L57L17a. Effects of canard surface size on stability and control characteristics of 2 canard airplane configurations at Mach nos. 1.41 and 2.01 [with list of references]; by M. Leroy Spearman and Cornelius Driver.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

325. NACA research memorandum RM (series). L58A07. Investigation of longitudinal aerodynamic characteristics of trapezoidal-wing airplane model with various vertical positions of wing and horizontal tail at Mach numbers of 1.41 and 2.01 [with list of references); by Gerald V. Foster.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

326. NACA research memorandum RM (series). L58A08. Investigation of high-flow transonic-compressor Inlet stage having hubtip radius ratio of 0.85 [with list of references;; by A. Richard Felix.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 6, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

327. NACA research memorandum RM (series). E57J17. Experimental investigation of effect of circumferential inlet flow distortion on performance of 5-stage axial-flow research compressor with transonic rotors in all stages [with list of references]; by William H. Robbins and Frederick Glaser.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 5, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

328. NACA research memorandum RM (series). E57K19b. Investigation at supersonic speeds of compressor stall and inlet buzz characteristics of J34-spike-inlet combination [with list of references]; by J. Cary Nettles and Robert C. Campbell.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 5, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

329. NACA research memorandum RM (series). E57L06. Performance of 2-dlmensional cascade inlet at free-stream Mach number of 3.05 and at angles of attack of —3°. 0°. 3°. and 6° [with list of references]: by Richard R. Woollett and Harold M. Ferguson.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Mar. 5, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

330. NACA research memorandum RM (series). A57L11a. Effects of modified roll-command system on flight-path stability and tracking accuracy of automatic interceptor [with list of references]; by William C Triplett.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Washington, Mar. 4, 1958
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

« Previous
Next »
1
2
…
29
30
31
32
33 Current Page, Page 33
34
35
36
37
…
111
112