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NASA Technical Note [D-2701-2710] (Record no. 565844)

000 -LEADER
fixed length control field 02489nam a22002777a 4500
003 - CONTROL NUMBER IDENTIFIER
control field OSt
040 ## - CATALOGING SOURCE
Transcribing agency IIT Kanpur
041 ## - LANGUAGE CODE
Language code of text/sound track or separate title eng
245 ## - TITLE STATEMENT
Title NASA Technical Note [D-2701-2710]
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication Washington
Name of publisher National Aeronautics and Space Administration (NASA)
Year of publication 1965
490 ## - SERIES STATEMENT
Series statement National Aeronautics and Space Administration (NASA)
-- NASA Technical Note
500 ## - GENERAL NOTE
General note NASA TN D-2701: Effects of Lateral control, characteristics on hovering: jet lift vtol aircraft/ by L. Stewart Rolls, Fred J. Drinkwater III and Robert C. Innis
500 ## - GENERAL NOTE
General note NASA TN D-2702: Impact of V / STOL aircraft on instrument weather operations/ John P. Reeder
500 ## - GENERAL NOTE
General note NASA TN D-2703: Description and initial calibration of the langley 12-inch Hypersonic ceramic-heated tunnel/ Louis E. Clark
500 ## - GENERAL NOTE
General note NASA TN D-2704: Hemispherical spectral emittance of ablation chars, carbon, and zirconia to 3700 degree K / by R. Gale Wilson
500 ## - GENERAL NOTE
General note NASA TN D-2705: results of USAF-NASA-FAA flight program to study community responses to sonic booms in the greater St. Louis Area/ by Charles W. Nixon, Harvey H. Hubbard
500 ## - GENERAL NOTE
General note NASA TN D-2706: Effect of surface emittance on turbulent skin friction at supersonic and low hypersonic speeds/ Jerry M. Allen and K. R. Czarnecki
500 ## - GENERAL NOTE
General note NASA TN D-2707: Fixed- base simulator study of piloted entry into the earth's atmosphere at parabolic velocity/ by Martin T. Moul and Albert A. Schy
500 ## - GENERAL NOTE
General note NASA TN D-2708: Study of pressure and heat transfer over an 80 degree sweep slab delta wing in hypersonic flow/ Allen H. Whitehead and James C. Dunavant
500 ## - GENERAL NOTE
General note NASA TN D-2709: Effect of first-stage geometry on aerdynamic characteristics in pitch of two-stage rocket vehicles from mach 1.57 to 2.86/ by William A. Corlett and Celia S. Richardson
500 ## - GENERAL NOTE
General note NASA TN D-2710: Effect of combined linear and oscillatory acceleration on pilot attitude-control capabilities/by Constantine B. Dolkas and John D. Stewart
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical Term Hypersonic Ceramic-Heated
653 ## - INDEX TERM--UNCONTROLLED
Uncontrolled term Pilots Evaluation--NASA
-- Pilots Evaluation--NASA
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Rolls, L. Stewart
-- Drinkwater III, Fred J.
-- Innis, Robert C.
-- Reeder, John P.
-- Clark, Louis E.
-- Wilson, R. Gale
-- Nixon, Charles W.
-- Hubbard, Harvey H.
-- Allen, Jerry M.
-- Czarnecki, K. R.
-- Moul, Martin T.
-- Schy, Albert A.
-- Whitehead, Allen H.
-- Dunavant, James C.
-- Corlett, William A. and
-- Richardson, Celia S.
-- Dolkas, Constantine B.
-- Stewart, John D.
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type Books
Holdings
Withdrawn status Lost status Damaged status Not for loan Collection code Permanent Location Current Location Date acquired Serial Enumeration / chronology Accession Number Koha item type
        COMPACT STORAGE (BASEMENT) PK Kelkar Library, IIT Kanpur PK Kelkar Library, IIT Kanpur 2022-07-07 NASA TN D2701-2710 64273 Technical Report

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