Books by Ames Research Center
Aircraft Configurations Develo
Aircraft Configurations Developing High Lift-Drag Ratios at High Supersonic Speeds
Comparison of Measured and Pre
Comparison of Measured and Predicted Indicated Angles of Attack near the Fuselages of a Triangular-Wing Wind-tunnel Model and a Swept-wing Fighter Airplane in Flight
Preliminary Report on a Study
Preliminary Report on a Study of Separated Flows in Supersonic and Subsonic Streams
Exobiology in Earth Orbit
Pseudo-Aircraft Systems
Pseudo-Aircraft Systems
1996 NASA-ASEE-Stanford Summer
1996 NASA-ASEE-Stanford Summer Faculty Fellowship Program
NAS technical summaries, March
NAS technical summaries, March 1993-February 1994
Studying turbulence using nume
Studying turbulence using numerical simulation databases
Methodologies for processing p
Methodologies for processing plant material into acceptable food on a small scale, phase II
NASA/Army rotorcraft technolog
NASA/Army rotorcraft technology
Research and technology, annua
Research and technology, annual report 1987
Some innovations and accomplis
Some innovations and accomplishments of Ames Research Center since its inception
Analysis of the Gran Desierto-
Analysis of the Gran Desierto-Pinacate region, Sonora, Mexico, via shuttle imaging radar
Long life feasibility study fo
Long life feasibility study for the shuttle infrared telescope facility
Studies in astronomical time s
Studies in astronomical time series analysis
Symposium on Recent Results in
Symposium on Recent Results in Infrared Astrophysics
A Forecast of space technology
A Forecast of space technology, 1980-2000
Systems reliability issues for
Systems reliability issues for future aircraft
A Primer in lunar geology
A Primer in lunar geology
Developments in laser technolo
Developments in laser technology, II
Outer planet entry probe techn
Outer planet entry probe technical summary
Method for simulating the atmo
Method for simulating the atmospheric entry of long-range ballistic missiles
Temperature Recovery Factors o
Temperature Recovery Factors on a Slender 12° Cone-Cylinder at Mach Numbers from 3. 0 to 6. 3 and Angles of Attack up To 45°
On the range of applicability
On the range of applicability of the transonic area rule
Comparison of the Experimental
Comparison of the Experimental and Theoretical Distributions of Lift on a Slender Inclined Body of Revolution at M = 2
Effect of bluntness on the dra
Effect of bluntness on the drag of spherical-tipped truncated cones of fineness ratio 3 at Mach numbers 1.2 to 7.4
Experimental Investigation of
Experimental Investigation of the Effects of Viscosity on the Drag of Bodies of Revolution at a Mach Number Of 1. 5