Publisher: National Aeronautics and Space Administration / Catalog Issue Year Decade: 1960 - 1969 - Blacklight Search Results

Start Over Publisher National Aeronautics and Space Administration Catalog Issue Year Decade 1960 - 1969

9921. NASA technical memorandums. X-105. Investigation at Mach numbers of 0.20 to 3.50 of blended diamond wing and body combination of sonic design but with low wave-drag increase with increasing Mach number [with list of references]; by George H. Holdaway, Jack A. Mellenthin, and Elaine W. Hatfield.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1959
SuDoc number:: NAS 1.15:(letters-nos.)

9922. NASA technical memorandums. X-123. Effect of wing thickness and sweep on oscillating hinge-moment and flutter characteristics of flap-type control at transonic speeds [with list of references]; by William C. Moseley, jr., and Thomas G. Gainer.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1959
SuDoc number:: NAS 1.15:(letters-nos.)

9923. NASA technical memorandums. X-141. Static stability characteristics of 3 thick wing models with parabolic plan forms at Mach number of 3.11 [with list of references];by M. J. Queijo.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1959
SuDoc number:: NAS 1.15:(letters-nos.)

9924. NASA technical memorandums. X-207. Measurements obtained during 1st landing of North American X-15 research airplane [with one reference]; by James M. McKay.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1959
SuDoc number:: NAS 1.15:X-(nos.)

9925. NASA technical memorandums. X-92. Effects of wing-crank, leading-edge chord extensions and horizontal-tall height on longitudinal stability of swept-wing models at Mach numbers from 0.6 to 1.4 [with list of references]; by Roy M. Wakefield.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Oct. 1959
SuDoc number:: NAS 1.15:(letters-nos.)

9926. NACA research memorandum RM (series). L54G22. Effect of yaw and angle of attack on pressure recovery and mass-flow characteristics of rectangular supersonic scoop inlet at Mach number of 2.71 [with list of references]; by Raymond J. Comenzo and Ernest A. Mackley.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 10, 1959
SuDoc number:: Y 3.N 21/5:15/(letter-nos.)

9927. NASA technical memorandum TM (series). X-119. Aerodynamic loading characteristics including effects of aeroelasticity of thin-trapezoidal-wing-body combination at Mach number of 1.43 [with list of references]; by Thomas C. Kelly.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1959
SuDoc number:: NAS 1.15:X-119

9928. NASA technical memorandum TM (series). X-137. Flight behavior of X-2 research airplane to Mach number of 3.20 and geometric altitude of 126,200 feet [with list of references]; by Richard E. Day and Donald Reisert.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1959
SuDoc number:: NAS 1.15:(letter-nos.)

9929. NASA technical memorandum TM (series). X-75. Experimental and analytical study of rolling-velocity amplification during thrusting process for 2 10-inch-dlameter spherical rocket motors in free flight [with one reference]; by C. William Martz and Robert L. Swain.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1959
SuDoc number:: NAS 1.15:(letter-nos.)

9930. NASA technical memorandums TM (series). X-16. Investigation of 0.05-scale model of XSM-64A Navaho missile and booster at supersonic Mach numbers: pt. 1, Force study [with one reference]; by James D. Church and Nancy L. Taylor.

Corporate/Agency Authors:: National Aeronautics and Space Administration
Publisher:: National Aeronautics and Space Administration
Date:: Sept. 1959
SuDoc number:: NAS 1.15:X-(nos.)

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