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EFFECTS OF TWO PROBE ANTENNAS ON AERODYNAMIC CHARACTERISTICS OF APOLLO SPACECRAFT AT MACH 10.03

by Putnam, Lawrence E.

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Washington 1967 National Aeronautics and Space Administration. 4to., 17pp., photo illustrations, wraps. Institution stamps on front and rear wrap. VG. .
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EXPERIMENTAL PRESSURE DISTRIBUTIONS ON A 120 (degree) CONE AT MACH NUMBERS FROM 2.96 TO 4.63 AND ANGLES OF ATTACK FROM 0 (degrees) TO 20 (degrees)

by Stallings, Robert L. Jr. and Dorothy H. Tudor

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Washington 1969. National Aeronautics and Space Administration TN D-5054. 4to., 76pp., wraps. A few institution names stamped on front. Mailing label affixed to rear wrap. VG. .
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FULL-SCALE INVESTIGATION OF THE AERODYNAMIC CHARACTERISTICS OF A SAILWING OF ASPECT RATIO 5.9

by Fink, Marvin P

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Washington 1969 National Aeronautics and Space Administration. 4to., 30pp., wraps. Institution stamp on front. VG. .
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A NUMERICAL METHOD FOR EVALUATION AND UNTILIZATION OF SUPERSONIC NACELLE-WING INTERFERENCE

by Mack, Robert J

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Washington 1969. National Aeronautics and Space Administration TN D-5057. 4to., 26pp., wraps. A few institution names stamped on front. Mailing label affixed to rear wrap. VG. .
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