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From the NTRS FAQ: Where do I go for a hardcopy of the report?

  1. MEASUREMENTS OF THE WING AND TAIL LOADS DURING THE ACCEPTANCE TESTS OF THE BELL XS-1 RESEARCH AIRPLANE , Research Memorandum
    Authors: De E. Beeler and John P. Mayer
    Report Number: NACA-RM-L7L12
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
    Currently this document is not available on-line.
    From the NTRS FAQ: Where do I go for a hardcopy of the report?
    Report Date: April 1948
  2. RESULTS OBTAINED DURING ACCELERATED TRANSONIC TESTS OF THE BELL XS-1 AIPLANE IN FLIGHTS TO A MACH NUMBER OF 0.92
    Authors: Huber M. Drake, Milton D. McLaughlin and Harold R. Goodman
    Report Number: NACA-RM-L8A05A
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          Postscript (9,218 KBytes)
          PDF (1,647 KBytes)
    Report Date: January 1948
    No. Pages: 24
  3. RESULTS OF PRELIMINARY FLIGHT TESTS OF THE XS-1 AIRPLANE (8-PERCENT WING) TO A MACH NUMBER OF 1.25 , Reserarch Memorandum
    Authors: Walter C. Williams and De Elroy Beeler
    Report Number: NACA-RM-L8A09
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
    Currently this document is not available on-line.
    From the NTRS FAQ: Where do I go for a hardcopy of the report?
    Report Date: April 1948
  4. RESULTS OF PRELIMINARY FLIGHT TESTS OF THE XS-1 AIRPLANE (8-PERCENT WING) TO A MACH NUMBER OF 1.25
    Authors: W. C. Williams and De E. Beeler
    Report Number: NACA-RM-L8A23A
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          Postscript (6,389 KBytes)
          PDF (1,087 KBytes)
    Report Date: April 1948
    No. Pages: 17
  5. RESULTS OBTAINED DURING A DIVE RECOVERY OF THE BELL XS-1 AIRPLANE TO HIGH LIFT COEFFICIENTS AT A MACH NUMBER GREATER THAN 1.0
    Authors: Milton D. McLaughin and Dorothy C. Clift
    Report Number: NACA-RM-L8C23A
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          Postscript (2,216 KBytes)
          PDF (576 KBytes)
    Report Date: April 1948
    No. Pages: 8
  6. LIMITED MEASUREMENTS OF STATIC LONGITUDINAL STABILITY IN FLIGHT OF DOUGLAS D-558-1 AIRPLANE
    Authors: Walter C. Williams
    Report Number: NACA-RM-L8E14
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          Postscript (3,499 KBytes)
          PDF (409 KBytes)
    Report Date: June 1948
    No. Pages: 10
  7. EFFECT OF DOWNWASH ON THE ESTIMATED ELEVATOR DEFLECTION REQUIRED FOR TRIM OF THE XS-1 AIRPLANE
    Authors: Jmes T. Matthews, Jr.
    Report Number: NACA-RM-L8H06A
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          Postscript (4,685 KBytes)
          PDF (569 KBytes)
    Report Date: November 1948
    No. Pages: 12
  8. RESULTS OBTAINED DURING EXTENSION OF U.S. AIR FORCE TRANSONIC-FLIGHT TESTS OF XS-1 AIRPLANE
    Authors: Harold R. Goodman and Hubert M. Drake
    Report Number: NACA-RM-L8I28
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          Postscript (5,323 KBytes)
          PDF (1,472 KBytes)
    Report Date: November 1948
    No. Pages: 14
  9. PRELIMINARY RESULTS OF NACA TRANSONIC FLIGHTS OF THE XS-1 AIRPLANE WITH 10-PERCENT-THICK WING AND 8-PERCENT-THICK HORIZONTAL TAIL
    Authors: Hubert M. Drake, Harold R. Goodman and Herbert H. Hoover
    Report Number: NACA-RM-L8I29
    Performing Organization: NASA Dryden Flight Research Center, Edwards, CA
    Availability:
        Format(s) on-line:
          Postscript (4,837 KBytes)
          PDF (1,359 KBytes)
    Report Date: October 1948
    No. Pages: 19