Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8êto 90ê
By: prepared for Langley Research Center under contract NAS1-14849
Contributors: Hultberg, Randy S; Mulcay, William; Bihrle, William; Rose, Robert A; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office; Langley Research Center
Series: NASA contractor report -- 3100-3102
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1979
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Subjects: Aerodynamics
Notes: Volumes 2 & 3 published by the NASA Scientific and Technical Information Branch

Includes bibliographical references
Table of contents: value: v. 1. Low-wing model A / Randy S. Hultberg and William Mulcay; value: v. 2. High-wing model A / William Mulcay and Robert Rose; value: v. 3. Effect of wing leading-edge modifications model A / William Bihrle, Jr., and William Mulcay