Prediction of forces and moments for flight vehicle control effectors
By: M. Maughmer ... [et al.].
Contributors: Maughmer, Mark D.; Langley Research Center.
Series: NASA contractor report -- NASA CR-186571.; NASA contractor report -- NASA CR-186572.
Publisher: National Aeronautics and Space Administration, Langley Research Center
Published: 1990
Place of publication: Hampton, VA
Language: eng
Format: Microform
Subjects: Aerodynamic characteristics.; Aerodynamic configurations.; Aerodynamic stability.; Aerodynamics.; Ailerons.; Aircraft configurations.; Computer programs.; Control equipment.; Control surfaces.; Delta wings.; Ground effect (Aerodynamics); Hypersonic aircraft.; Hypersonics.; Planforms.; Predictions.; Rudders.; Space shuttle orbiters.; X-15 aircraft.
Notes: Shipping list no.: 1990-0881-M (v. 1 and 2).

Distributed to depository libraries in microfiche.

"NASA grant NAG 1-849."

"May 1990."

Includes bibliographical references.

Also available via Internet from the NTRS web site. Addresses as of 4/25/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012418%5F1990012418.pdf (v. 1) and http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900012419%5F1990012419.pdf (v. 2); current access is available via PURLs.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1990. 4 microfiches.
Table of contents: title: v. 1. Validation of methods for predicting hypersonic vehicle controls forces and moments; title: v. 2. An analysis of delta wing aerodynamic control effectiveness in ground effect.